G1000TM Cockpit Reference Guide for the Diamond DA40

This manual reﬂects the operation of System Software version 0369.10 or later for the Diamond DA40, DA40F. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282 Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A. Tel: 503/391.3411 Fax 503/364.2138 Garmin (Europe) Ltd., Unit 5, The Quadrangle, Abbey Park Industrial Estate, Romsey, Hampshire S051 9DL, U.K. Tel: 44/0870.8501241 Fax: 44/0870.8501251 Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan Tel: 886/02.2642.9199 Fax: 886/02.2642.9099 Web Site Address: www.garmin.com Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited. Garmin® is a registered trademark of Garmin Ltd. or its subsidiaries, and G1000™ is a trademark of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin. NavData® is a registered trademark of Jeppesen, Inc.; Stormscope® is a registered trademark of L-3 Communications; and XM® is a registered trademark of XM Satellite Radio, Inc.

May 2006 190-00324-05 Rev. A Printed in the U.S.A.

Garmin G1000 Cockpit Reference Guide for the DA40 WARNINGS, CAUTIONS, & NOTES

WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function. The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system. Terrain data is obtained from third party sources. Garmin is not able to independently verify the accuracy of the terrain data.

WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical charts for appropriate minimum clearance altitudes.

WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary signiﬁcantly from the altitude displayed by pressure altimeters, such as the GDC 74A Air Data Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.

WARNING: The Jeppesen database used in the G1000 system must be updated regularly in order to ensure that its information remains current. Updates are released every 28 days. A database information packet is included in the G1000 package. Pilots using an outdated database do so entirely at their own risk.

WARNING: The basemap (land and water data) must not be used for navigation, but rather only for non- navigational situational awareness. Any basemap indication should be compared with other navigation sources.

WARNING: Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic. Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic.

WARNING: Use of the Stormscope is not intended for hazardous weather penetration (thunderstorm penetration). Stormscope information, as displayed on the G1000 MFD, is to be used only for weather avoidance, not penetration.

WARNING: XM Weather should not be used for hazardous weather penetration. Weather information provided by the GDL 69 is approved only for weather avoidance, not penetration.

Garmin G1000 Cockpit Reference Guide for the DA40 WARNINGS, CAUTIONS, & NOTES

WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range weather avoidance.

WARNING: The Garmin G1000, as installed in the Diamond DA40 aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated information available in the cockpit.

WARNING: For safety reasons, G1000 operational procedures must be learned on the ground.

WARNING: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be misused or misinterpreted and, therefore, become unsafe.

WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000 Pilot’s Guide documentation and the G1000 Flight Manual Supplement. Thoroughly practice basic operation prior to actual use. During ﬂight operations, carefully compare indications from the G1000 to all available navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation.

WARNING: The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Airman’s Information Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identiﬁed as severe or giving an intense radar echo.”

CAUTION: The GDU 1040 PFD and GDU 1042 MFD displays use a lens coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti-reflective coatings.

Garmin G1000 Cockpit Reference Guide for the DA40 WARNINGS, CAUTIONS, & NOTES

CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modiﬁcations could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations.

NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode. However, clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleared.

NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and displays, are subject to change and may not reﬂect the most current G1000 system. Depictions of equipment may differ slightly from the actual equipment.

NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) this device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation.

NOTE: All references to the Diamond DA40 aircraft equally apply to the Diamond DA40F aircraft, unless otherwise noted.

NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65.

Garmin G1000 Cockpit Reference Guide for the DA40 RECORD OF REVISIONS

Part Number Change Summary 190-00324-00 Initial Release Rev. A 190-00324-01 Reformat of manual Rev. A Added NAV/COM volume levels Added Flight Timer Added extended range fuel tanks Changed NAV1 and NAV2 on the PFD to VOR or LOC Moved altitude and airspeed trend vectors to opposite sides 190-00324-02 Added WX 500 Stormscope Rev. A Added XM Weather Added ADF/DME Added bearing pointers Added ﬁxed pitch propeller engine parameters 190-00324-02 Updated ﬁxed pitch propeller engine parameters. Rev. B Added reference to DA40F on Copyright page and in Warnings, Cautions, and Notes 190-00324-03 Added diesel engine parameters Rev. A 190-00324-04 Added fuel pressure gauge for the DA40 Rev. A 190-00324-05 Added GFC 700 Automatic Flight Control System Rev. A Added GDU 6.10 software parameters Updated G1000 System Messages Removed diesel engine parameters

Revision Date of Revision Affected Pages Description A 5/06 i-Index-2 Production Release

Garmin G1000 Cockpit Reference Guide for the DA40 RR-1 RECORD OF REVISIONS

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RR-2 Garmin G1000 Cockpit Reference Guide for the DA40 TABLE OF CONTENTS

SECTION 1: SYSTEM OVERVIEW ...... 1-1 4.6 Frequency Auto-tuning ...... 4-4 1.1 PFD/MFD Controls ...... 1-2 Auto-tuning on the PFD ...... 4-4 1.2 PFD Softkeys ...... 1-4 Auto-tuning on the MFD ...... 4-4 1.3 MFD Softkeys ...... 1-7 4.7 Transponder ...... 4-5 1.4 MFD Page Groups ...... 1-8 Mode Selection ...... 4-5 1.5 Backlighting ...... 1-8 Ground Mode (Automatic) ...... 4-5 Reply Status ...... 4-5 SECTION 2: FLIGHT INSTRUMENTS ...... 2-1 Code Selection ...... 4-5 2.1 Airspeed Indicator ...... 2-3 Flight ID Reporting ...... 4-5 Speed Indication ...... 2-3 Speed Ranges ...... 2-3 SECTION 5: AUDIO PANEL ...... 5-1 Airspeed Trend Vector ...... 2-3 5.1 COM Radio Selection ...... 5-2 Vspeed References ...... 2-3 5.2 Marker Beacon Receiver ...... 5-2 2.2 Attitude Indicator ...... 2-3 Marker Beacon Signal Sensitivity ...... 5-2 2.3 Altimeter ...... 2-4 5.3 Nav Radio Audio Selection ...... 5-2 Altitude Select Bug ...... 2-4 5.4 Intercom System (ICS) Isolation ...... 5-3 Altitude Trend Vector ...... 2-4 5.5 Intercom Squelch Control ...... 5-3 Barometric Setting Box ...... 2-4 5.6 Digital Clearance Recorder and Player ...... 5-4 Altitude Alerting ...... 2-4 Barometric Minimum Descent Altitude ...... 2-4 SECTION 6: AUTOMATIC FLIGHT CONTROL ...... 6-1 2.4 Marker Beacon Annunciations ...... 2-5 6.1 Mode Annunciations ...... 6-1 2.5 Vertical Deviation/Glideslope Indicator ...... 2-5 6.2 Overspeed Protection ...... 6-2 2.6 Vertical Speed Indicator ...... 2-5 6.3 AP Engagement/Disengagement ...... 6-2 2.7 Horizontal Situation Indicator (HSI) ...... 2-5 Automatic Disengagement ...... 6-3 Course Pointer ...... 2-6 Manual Disengagement ...... 6-3 Course Deviation Indicator (CDI) ...... 2-7 Control Wheel Steering ...... 6-3 Bearing Pointers and Information Windows ...... 2-7 6.4 Loss of Data ...... 6-3 DME (optional) ...... 2-7 6.5 Pitch Axis Modes ...... 6-3 Navigation Source ...... 2-7 Pitch Hold Mode (PIT) ...... 6-4 Altitude Hold Mode (ALT) ...... 6-5 SECTION 3: ENGINE INDICATION SYSTEM (EIS) .... 3-1 Vertical Speed Mode (VS) ...... 6-6 3.1 Engine Display ...... 3-1 Flight Level Change Mode (FLC) ...... 6-7 Fuel Pressure Indicator (Option, DA40 only) ...... 3-1 Go-Around Mode (GA) ...... 6-8 3.2 Lean Engine Display ...... 3-2 Glideslope (GS) ...... 6-8 Cylinder Select ...... 3-2 6.6 Roll Axis Modes ...... 6-9 3.3 Engine System Display ...... 3-3 Roll Hold Mode (ROL) ...... 6-9 Heading Select Mode (HDG) ...... 6-10 SECTION 4: NAV/COM AND TRANSPONDER ...... 4-1 Navigation Mode (GPS, VOR, LOC, or BC) ...... 6-11 4.1 Radio Status Indications ...... 4-3 Navigation Mode Armed ...... 6-11 4.2 Volume ...... 4-3 Approach Mode (GPS, VAPP or LOC) ...... 6-12 4.3 Automatic Squelch ...... 4-3 Go Around (GA) ...... 6-12 4.4 Quickly Activating 121.500 MHz ...... 4-3 6.7 Example Procedures Using AFCS ...... 6-13 4.5 Optional NAV Radios ...... 4-3 Departure ...... 6-14 ADF Radio (optional) ...... 4-3 Intercepting a VOR Radial ...... 6-15 DME Radio (optional) ...... 4-4

Garmin G1000 Cockpit Reference Guide for the DA40 i TABLE OF CONTENTS

Flying a GPS Flight Plan ...... 6-16 Load an Airport COM Frequency into the Flight Level Change (Descent) ...... 6-17 Active COM ...... 7-6 ILS Approach ...... 6-18 7.9 Nearest Intersections ...... 7-7 Go-Around / Missed Approach ...... 6-19 Select the Nearest Intersections Page ...... 7-7 View Information on the Nearest Intersection ...... 7-7 SECTION 7: NAVIGATION ...... 7-1 7.10 Nearest NDB ...... 7-7 7.1 Navigation Map Page ...... 7-1 Select the Nearest NDB Page ...... 7-7 Select the MAP Page Group ...... 7-1 Access Information on a Specific NDB ...... 7-7 7.2 Direct-to Navigation ...... 7-1 7.11 Nearest VOR ...... 7-8 Direct-to Navigation from the MFD ...... 7-1 Select the Nearest VOR Page ...... 7-8 Enter a Direct-to Destination ...... 7-1 View Information on the Nearest VOR ...... 7-8 Select a Direct-to Destination to a Flight Plan Select and Load a VOR Frequency ...... 7-8 Waypoint or Nearest Airport ...... 7-1 7.12 Nearest User Waypoint ...... 7-8 To Re-center the CDI to the Destination Waypoint ... 7-2 Select the Nearest User Waypoint Page ...... 7-8 To Manually Define the Direct-to Course ...... 7-2 Select a Nearest User Waypoint ...... 7-8 Canceling Direct-to Navigation ...... 7-2 7.13 Nearest Frequencies ...... 7-9 Direct-to Navigation from the PFD ...... 7-2 Select the Nearest Frequencies Page ...... 7-9 Cancelling Direct-to Navigation ...... 7-2 Select and Load the Nearest ARTCC, FSS, or 7.3 Airport Information ...... 7-3 Weather Frequency ...... 7-9 Select the Airport Information Page ...... 7-3 7.14 Nearest Airspaces ...... 7-9 Enter a Waypoint Facility Name or City Location ...... 7-3 Select the Nearest Airspaces Page ...... 7-9 Access Runway Information ...... 7-3 Airspace Alerts Box ...... 7-9 Access Frequency Information ...... 7-3 View Additional Details for a Listed Airspace ...... 7-10 7.4 Intersection Information ...... 7-4 View and Quickly Load the Frequency for a Select the Intersection Information Page ...... 7-4 Controlling Agency ...... 7-10 Access Information on an Intersection ...... 7-4 7.5 NDB Information ...... 7-4 SECTION 8: FLIGHT PLANNING ...... 8-1 Select the NDB Information Page ...... 7-4 8.1 User Defined Waypoints ...... 8-1 View Information on a Specific NDB ...... 7-4 Select the User WPT Information Page ...... 8-1 7.6 VOR Information ...... 7-5 Create a New User Waypoint ...... 8-1 Select the VOR Information Page ...... 7-5 Modify a User Waypoint ...... 8-1 Access Information on a VOR ...... 7-5 Delete a User Waypoint ...... 8-1 7.7 User Waypoint Information Page ...... 7-5 Create User Waypoints from the Navigation 7.8 Nearest Airports ...... 7-5 Map Page ...... 8-2 Nearest Airport Information on the MFD ...... 7-5 8.2 Viewing the Active Flight Plan ...... 8-2 Select the Nearest Airports Page ...... 7-5 8.3 Activate a Stored Flight Plan ...... 8-2 Access Information on a Specific Airport ...... 7-5 8.4 Activate a Flight Plan Leg ...... 8-3 Access Runway Information for the 8.5 Stop Navigating a Flight Plan ...... 8-3 Selected Airport ...... 7-6 8.6 Invert Active Flight Plan ...... 8-3 Quickly Tune the COM Transceiver to a Nearby Airport 8.7 Create a New Flight Plan ...... 8-3 Frequency ...... 7-6 Create a New Flight Plan Using the MFD ...... 8-3 Nearest Airports Information on the PFD ...... 7-6 Create a New Flight Plan Using the PFD ...... 8-4 View Information on a Specific Airport in the List .... 7-6 8.8 Load a Departure ...... 8-4 8.9 Load an Arrival ...... 8-4 ii Garmin G1000 Cockpit Reference Guide for the DA40 TABLE OF CONTENTS

8.10 Load an Approach ...... 8-5 SECTION 11: ABNORMAL OPERATION ...... 11-1 8.11 Remove a Departure, Arrival, or Approach 11.1 Reversionary Mode ...... 11-1 from a Flight Plan ...... 8-5 11.2 Abnormal COM Operation ...... 11-2 8.12 Store a Newly Created Flight Plan ...... 8-5 11.3 Unusual Attitudes ...... 11-2 8.13 Edit a Stored Flight Plan ...... 8-5 11.4 Stormscope operation with loss of 8.14 Delete a Waypoint from the Flight Plan ...... 8-5 Heading Input ...... 11-2 8.15 Invert and activate a Stored Flight Plan ...... 8-6 11.5 Hazard Displays with Loss of GPS Position .... 11-2 8.16 Copy a Flight Plan ...... 8-6 8.17 Delete a Flight Plan ...... 8-6 SECTION 12: ANNUNCIATIONS & ALERTS ...... 12-1 8.18 Graphical Flight Plan Creation ...... 8-6 12.1 Alert Level Definitions ...... 12-2 8.19 Trip Planning ...... 8-6 12.2 Aircraft Alerts ...... 12-3 8.20 Vertical Navigation (VNAV) Page ...... 8-8 WARNING Alerts ...... 12-3 Create a Vertical Navigation Profile ...... 8-8 CAUTION Alerts ...... 12-3 VNAV Page Menu Options ...... 8-9 Message Advisory Alerts ...... 12-3 12.3 AFCS Alerts ...... 12-4 SECTION 9: PROCEDURES ...... 9-1 System Status Annunciation ...... 12-4 9.1 Arrivals and Departures ...... 9-1 12.4 G1000 System Annunciations ...... 12-5 Load and Activate a Departure Procedure ...... 9-1 12.5 G1000 System Message Advisories ...... 12-7 Load and Activate an Arrival Procedure ...... 9-1 MFD & PFD Message Advisories ...... 12-8 9.2 Approaches ...... 9-2 Database Message Advisories ...... 12-9 Load and/or Activate an Approach Procedure ...... 9-2 GMA 1347 Message Advisories ...... 12-10 Activate An Approach in the Active Flight Plan ...... 9-3 GIA 63 Message Advisories ...... 12-10 GEA 71 Message Advisories ...... 12-12 SECTION 10: HAZARD AVOIDANCE ...... 10-1 GTX 33 Message Advisories ...... 12-13 10.1 Customizing the Hazard Displays on the GRS 77 Message Advisories ...... 12-13 Navigation Map ...... 10-1 GMU 44 Message Advisories ...... 12-14 10.2 XM Weather (Optional) ...... 10-1 GDL 69 Message Advisories ...... 12-14 Displaying METAR and TAF information on the GDC 74A Message Advisories ...... 12-14 Airport Information Page ...... 10-1 Miscellaneous Message Advisories ...... 12-14 Displaying Weather on the Weather Data Link Page ... 10-2 NEXRAD Limitations ...... 10-2 INDEX ...... Index-1 Map Panning Information – Weather Data Link Page . 10-3 Weather Products and Symbols ...... 10-4 Weather Product Age ...... 10-4 10.3 Traffic Information Service (TIS) ...... 10-5 Displaying Traffic on the Traffic Map Page ...... 10-5 Displaying Traffic on the Navigation Map ...... 10-6 TIS Audio Alert ...... 10-6 10.4 Terrain And Obstacle Proximity ...... 10-6 Displaying Terrain and Obstacles on the Terrain Proximity Page ...... 10-6 Displaying Terrain and Obstacles on the Navigation Map ...... 10-7

Garmin G1000 Cockpit Reference Guide for the DA40 iii TABLE OF CONTENTS

iv Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 1 SYSTEM OVERVIEW

SECTION 1: SYSTEM OVERVIEW This guide gives the pilot abbreviated operating instructions for the Primary Flight Display (PFD), Multi The purpose of this Cockpit Reference Guide is to Function Display (MFD), and the GMA 1347 Audio Panel provide the pilot a resource with which to ﬁnd operating System. instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive NOTE: The pilot should read and thoroughly operating guide. Complete operating procedures for the understand the Diamond DA40 Aircraft Flight complete system are found in the G1000 Pilot’s Guide Manual Supplement (AFMS) for limitations, procedures and operational information not (190-00592-01). contained in this Cockpit Reference Guide. The Diamond DA40 Aircraft Flight Manual Supplement always takes precedence over the information found in this guide.

Garmin G1000 Cockpit Reference Guide for the DA40 1-1 SECTION 1 SYSTEM OVERVIEW

1.1 PFD/MFD CONTROLS

1 2 3 4 5 6 7 8 9

17 Figure 1-1 PFD/MFD Controls

18 10 14 19 24 11 15 20 25 12 16 21

22 26 13

23 27 MFD Only

1-2 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 1 SYSTEM OVERVIEW

PFD and MFD controls function the same with the (10) Direct-to Key – Allows the user to enter a destination exception of the dedicated Automatic Flight Control waypoint and establish a direct course to the selected System (AFCS) keys located only on the MFD bezel. destination (specified by the identifier, chosen from the active route, or taken from the map pointer position). (1) NAV VOL/ID Knob – Controls the NAV audio level. (11) FPL Key – Displays the active Flight Plan Page for Press to toggle the Morse code identifier ON and OFF. creating and editing the active flight plan, or for accessing Volume level is shown in the field as a percentage. stored flight plans. (2) NAV Frequency Toggle Key – Toggles the standby (12) CLR Key (DFLT MAP) – Erases information, and active NAV frequencies. cancels an entry, or removes page menus. To display the (3) Dual NAV Knob – Tunes the MHz (large knob) Navigation Map Page immediately, press and hold CLR and kHz (small knob) standby frequencies for the NAV (MFD only). receiver. Press to toggle the tuning cursor (light blue box) (13) Dual FMS Knob – Used to select the page to be between the NAV1 and NAV2 fields. viewed (only on the MFD). The large knob selects a page (4) Heading Knob – Turn to manually select a heading on the HSI. When pressed, it synchronizes the heading group (MAP, WPT, AUX, NRST), while the small knob bug with the compass lubber line. Selected Heading selects a specific page within the page group. Pressing the provides the heading reference to the Flight Director while small knob turns the selection cursor ON and OFF. When operating in Heading Select mode. the cursor is ON, data may be entered in the different (5) Joystick – Changes the map range (distance top to fields using the small and large knobs. The large knob is bottom of map display) when rotated. Activates the map used to move the cursor on the page, while the small knob pointer when pressed. is used to select individual characters for the highlighted (6) CRS/BARO Knob – The large knob sets the altimeter cursor location. When the G1000 displays a list that is barometric pressure and the small knob adjusts the too long for the display screen, a scroll bar appears along course. The course is only adjustable when the HSI is in the right side of the display, indicating the availability of VOR1, VOR2, or OBS/SUSP mode. Pressing this knob additional items within the selected category. Press the centers the CDI on the currently selected VOR. Selected small FMS Knob to activate the cursor and turn the large Course provides course reference to the Flight Director FMS Knob to scroll through the list. when operating in Navigation and Approach modes. (14) MENU Key – Displays a context-sensitive list of (7) Dual COM Knob – Tunes the MHz (large knob) options. This list allows the user to access additional and kHz (small knob) standby frequencies for the COM features, or to make setting changes that relate to certain transceiver. Pressing this knob toggles the tuning cursor pages. (light blue box) between the COM1 and COM2 fields. (15) PROC Key – Selects approaches, departures and (8) COM Frequency Toggle Key – Toggles the standby arrivals from the flight plan. If a flight plan is used, and active COM frequencies. Pressing and holding this available procedures for the departure and/or arrival key for two seconds automatically tunes the emergency airport are automatically suggested. If a flight plan is not frequency (121.5 MHz) in the active frequency field. used, the desired airport and the desired procedure may be (9) COM VOL/SQ Knob – Controls COM audio level. selected. This key selects IFR departure procedures (DPs), Pressing this knob turns the COM automatic squelch ON arrival procedures (STARs) and approaches (IAPs) from and OFF. Audio volume level is shown in the field as a the database and loads them into the active flight plan. percentage. Garmin G1000 Cockpit Reference Guide for the DA40 1-3 SECTION 1 SYSTEM OVERVIEW

(16) ENT Key – Accepts a menu selection or data entry. (optional) This key is used to approve an operation or complete data INSET PFD OBS CDI ADF/DME XPDR IDENT TMR/REF NRST ALERTS entry. It is also used to confirm selections and information entries. Figure 1-2 PFD Top Level Softkeys (17) Dual ALT Knob – Sets the selected altitude in the INSET – Press to display the Inset Map in the lower box located above the Altimeter. The large knob selects left corner of the PFD. the thousands, while the small knob selects the hundreds. OFF – Press to remove the Inset Map. Altitude Select is used by the Automatic Flight Control DCLTR (3) – Press momentarily to select the desired System in certain modes, in addition to the standard amount of map detail. The declutter level appears G1000 Altitude Alerter function. adjacent to the DCLTR Softkey. (18) AP Key – Engages/disengages the Autopilot and • No declutter: All map features are visible Flight Director. Pressing the AP Key activates the Flight • Declutter – 1: Declutters land data Director and engages the Autopilot in the default pitch axis • Declutter – 2: Declutters land and SUA data and roll axis modes. Pressing the AP Key again disengages • Declutter – 3: Removes everything except the active the autopilot and deactivates the Flight Director. flight plan TRAFFIC – Press to display traffic on the inset map. (19) FD Key – Activates/deactivates the Flight Director TOPO – Press to display topographical data (i.e., FD only. Pressing the Key turns on the Flight Director in coastlines, terrain, rivers, lakes) and elevation the default pitch axis and roll axis modes. Pressing the scale on the inset map. FD key again deactivates the Flight Director and removes TERRAIN – Press to display terrain information on the command bars, unless the Autopilot is engaged. If the the inset map. Autopilot is engaged, the FD Key is disabled. STRMSCP (optional) – Press to display the (20) NAV Key – Selects/deselects the Navigation mode. Stormscope lightning data on the inset map (21) ALT Key – Selects/deselects the Altitude Hold (within a 200 nm radius of the aircraft). mode. NEXRAD (optional) – Press to display NEXRAD (22) VS Key – Selects/deselects the Vertical Speed mode. precipitation data on the inset map. (23) FLC Key – Selects/deselects the Flight Level Change XM LTNG (optional) – Press to display the XM Radio mode. lightning data on the inset map. (24) HDG Key – Selects/deselects the Heading Select BACK – Press to return to the previous level softkey configuration. mode. ALERTS – Press to display the Alerts Window. (25) APR Key – Selects/deselects the Approach mode. (26, 27) NOSE UP/NOSE DN Keys – Controls the PFD – Press to display the additional softkeys for active pitch reference for the Pitch Hold, Vertical Speed, additional configuration of the PFD. METRIC – Press to display the current and reference and Flight Level Change modes. altitudes in meters, in addition to feet. Pressing 1.2 PFD SOFTKEYS the metric softkey also changes the barometric setting to hectopascals. DFLTS – Press to reset default settings on the PFD. Softkey ON Softkey OFF DME (optional) – Press to display the DME Information Window.

1-4 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 1 SYSTEM OVERVIEW

BRG1 (bearing) – Press to cycle through the 360 HSI – Press to display the 360° compass rose. following Nav sources, making the pointer the ARC HSI – Press to display the 140° viewable arc. indicator for the corresponding source and displaying the the appropriate information. INSET

(optional) (optional) (optional) OFF DCLTR TRAFFIC TOPO TERRAIN STRMSCP NEXRAD XM LTNG BACK ALERTS

Press the BACK or OFF Softkey DCLTR-1 to return to the top level softkeys.

DCLTR-2

DCLTR-3

Figure 1-3 PFD Softkey Flow Chart – 1

PFD

(optional) METRIC DFLTS DME BRG1 360 HSI ARC HSI BRG2 STD BARO BACK ALERTS

Press the DFLTS Softkey to change the PFD Press the STD BARO or BACK Softkey metric values to standard to return to the top level softkeys

Figure 1-4 PFD Softkey Flow Chart – 2 NAV1 – Displays NAV1 waypoint frequency or BRG2 (bearing) – Press to cycle through the identifier and DME information in the BRG1 following Nav sources, making the pointer the Information Window. indicator for the corresponding source and GPS – Displays GPS waypoint identifier and GPS displaying the the appropriate information. distance information in the BRG1 Information NAV2 – Displays NAV2 waypoint frequency or Window. identifier and DME information in the BRG2 ADF – Displays ADF waypoint frequency in the Information Window. BRG1 Information Window. GPS – Displays GPS waypoint identifier and GPS OFF – Removes the BRG1 Information distance information in the BRG2 Information Window. Window.

Garmin G1000 Cockpit Reference Guide for the DA40 1-5 SECTION 1 SYSTEM OVERVIEW

ADF – Displays ADF waypoint frequency in the STBY – Press to select standby mode. BRG2 Information Window. ON – Press to select mode A. OFF – Removes the BRG2 Information ALT – Press to select altitude reporting mode. Window. VFR – Press to automatically squawk 1200 (only STD BARO – Press to set the barometric pressure to in the U.S.A., refer to ICAO standards for VFR 29.92 inches of mercury (1013 hPa by pressing codes in other countries). the METRIC Softkey). CODE – Press to display transponder code selection BACK – Press to return to the previous level softkeys 0-7. softkeys. 0 through 7 – Press numbers to enter code. ALERTS – Press to display the Alerts Window.

Press the BACK Softkey to return to the top level softkeys

Figure 1-5 PFD Softkey Flow ChartIDENT – 3 – Press to provide special aircraft OBS – Press to select OBS mode on the CDI when position identification to Air Traffic Control navigating by GPS (only available with active leg). (ATC). CDI – Press to change navigation mode on the CDI BKSP – Press to remove numbers entered one between GPS, VOR1, and VOR2. at a time. ADF/DME (optional) – Press to display the ADF/DME BACK – Press to return to the previous level Tuning Window. softkeys. XPDR – Press to display the transponder mode IDENT – Press to provide special aircraft position selection softkeys. identification to Air Traffic Control (ATC). 1-6 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 1 SYSTEM OVERVIEW

BACK – Press to return to the previous level softkeys. 1.3 MFD SOFTKEYS ALERTS – Press to display the Alerts Window. ENGINE – Pressing this softkey makes available IDENT – Press to provide special aircraft position the LEAN and SYSTEM Softkeys which in turn identiﬁcation to Air Trafﬁc Control (ATC). access the Lean Display and the System Display, TMR/REF – Press to display the Timer/References respectively. Window. MAP – Pressing this softkey enables the following NRST – Press to display the Nearest Airports softkeys: Window. ALERTS – Press to display the Alerts Window.

ENGINE MAP DCLTR CHKLIST

(optional)

Press the BACK Softkey on this level to return to the top softkey level DCLTR-1

ENGINE LEAN SYSTEM BACK DCLTR-2

DCLTR-3 Press to return to the top softkey level

(optional) (optional) (optional) TRAFFIC TOPO TERRAIN STRMSCP NEXRAD XM LTNG BACK

ENGINE LEAN SYSTEM DEC FUEL INC FUEL RST FUEL BACK

Press the ENGINE or BACK Softkey on any level to return to the default page level The DONE Softkey changes to UNDO when the checklist item is already checked ENGINE LEAN SYSTEM CYL SLCT ASSIST BACK ENGINE DONE EXIT EMERGCY

CLR

ENGINE MAP DCLTR CHKLIST

Figure 1-6 MFD Softkeys

Garmin G1000 Cockpit Reference Guide for the DA40 1-7 SECTION 1 SYSTEM OVERVIEW

TRAFFIC – Pressing this softkey displays/ 1.5 BACKLIGHTING removes Trafﬁc on the Navigation Map. TOPO – Pressing this softkey displays or When system power is turned off, all manual removes topographic information on the backlighting settings will return to the factory default Navigation Map. settings. TERRAIN – Pressing this softkey displays/ To manually adjust the backlight for the removes terrain and obstacle data on the PFD and MFD: Navigation Map. 1) Press the MENU Key on the PFD to display the STRMSCP (optional) – Pressing this softkey PFD Setup Menu Window. displays/removes Stormscope lightning data 2) Press the small FMS Knob to activate the cursor. on the Navigation Map. ‘PFD DSPL > AUTO’ is now highlighted. NEXRAD (optional) – Pressing this softkey displays/removes precipitation data on the 3) Turn the small FMS Knob to display the Navigation Map. selection window. XM LTNG (optional) – Pressing this softkey 4) Turn the FMS Knob to select ‘MANUAL’, then displays/removes XM Radio lightning data press the ENT Key. on the Navigation Map. 5) With the intensity value now highlighted, turn BACK – Pressing this softkey displays the the small FMS Knob to select the desired ENGINE and MAP top level softkeys. backlighting. DCLTR (declutter) – Pressing this softkey removes map information in three levels.

1.4 MFD PAGE GROUPS

1) Turn the large FMS Knob until the desired page group is selected. 2) Turn the small FMS Knob to select pages within the group. See Figure 1-7. Nearest Group

Auxiliary Page Group Number of Pages in Current Group Waypoint Page Group

Map Page Group

Figure 1-7 Page Group Icon Selected Page

1-8 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 1 SYSTEM OVERVIEW

6) Turn the large FMS Knob to highlight ‘MFD DSPL > AUTO’ and repeat steps 3 through 5.

Figure 1-8 PFD Setup Menu Window

Garmin G1000 Cockpit Reference Guide for the DA40 1-9 SECTION 1 SYSTEM OVERVIEW

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1-10 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 2 FLIGHT INSTRUMENTS

SECTION 2: FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display, unless otherwise indicated.

1 17 16 15 14

2 12

3 10

4 9

8 5

6 7

1 NAV Frequency Box 9 Turn Rate Indicator 2 Airspeed Indicator 10 Barometric Setting Box 3 True Airspeed Box 11 Vertical Speed Indicator 4 Heading Box 12 Altimeter 5 Horizontal Situation Indicator 13 Altitude Reference Box 6 Outside Air Temperature Box 14 COM Frequency Box 7 System Time Box 15 Navigation Status Box 8 Transponder Status Box 16 Slip/Skid Indicator 17 Attitude Indicator Figure 2-1 Default PFD Information

Garmin G1000 Cockpit Reference Guide for the DA40 2-1 SECTION 2 FLIGHT INSTRUMENTS

1 10

9 2 8

3 7

4 5 6

1 Trafﬁc Annunciation 7 Alerts Window 2 Selected Heading Box 8 Selected Course Box

3 Inset Map 9 Annunciation Window

4 BRG1 Information Window 10 Vertical Deviation/Glideslope Indicator 5 DME Information Window 11 Marker Beacon Annunciation 6 BRG2 Information Window Figure 2-2 Additional PFD Information

Desired Track to Distance to Next Waypoint Next Waypoint Current Track Next Waypoint

Figure 2-3 PFD Navigation Status Box

2-2 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 2 FLIGHT INSTRUMENTS

2.1 AIRSPEED INDICATOR Vspeed References Vspeed References are turned on or off in the Timer/References Window. Press the TMR/REF Softkey Airspeed Trend to display the widow. When active (ON), the Vspeeds are Vector displayed at their respective locations to the right of the Actual Airspeed airspeed scale. To activate the Vspeed References, display Vspeed the Timer/Reference Window and turn the large FMS References Knob to place the cursor in the ON/OFF ﬁeld. Turn the small FMS Knob to select ON or OFF. Speed Ranges True Airspeed Box 2.2 ATTITUDE INDICATOR Figure 2-4 Airspeed Indicator The Slip/Skid Indicator is located under the Roll Pointer and moves laterally away from the pointer to indicate Speed Indication lateral acceleration. One Slip/Skid indicator displacement The indicated airspeed is displayed inside the black is equal to one ball displacement when compared to a pointer. The pointer will become red upon reaching traditional slip/skid indicator. Vne. 10

9 1 8 2

Figure 2-5 Red Pointer at Vne 7 3 Speed Ranges 6 4 The color coded speed range strip denotes ﬂaps operating range, normal operating range, and never exceed 5 speed (Vne). A red range is also present for low speed awareness. Refer to the Airplane Flight Manual (AFM) for 1 Roll Pointer 6 Aircraft Wing Tips airspeed limitations and indicator markings. 2 Roll Scale 7 Pitch Scale Airspeed Trend Vector 3 Horizon Line The end of the trend vector displays approximately 8 Slip/Skid Indicator what the airspeed will be in 6 seconds if the current rate 4 Aircraft Symbol 9 Sky Representation of acceleration/deceleration is maintained. 5 Land Representation 10 Roll Index Zero

Figure 2-6 Attitude Indicator

Garmin G1000 Cockpit Reference Guide for the DA40 2-3 SECTION 2 FLIGHT INSTRUMENTS

2.3 ALTIMETER Altitude Alerting

Altitude Reference Within 1000 ft Within 200 ft Deviation of ±200 ft Box

Figure 2-8 Altitude Alerting Visual Annunciations

Altitude Trend Current Altitude Visual annunciations appear in the Selected Altitude Vector Box. Whenever the Selected Altitude is changed, the Altitude Alerter is reset. The Altitude Alerter is independent of the Automatic Flight Control System.

Altitude Select Bug Barometric Setting An aural tone is heard when the aircraft is within 1000 Box feet of acquiring the selected altitude or when deviating Figure 2-7 Altimeter beyond 200 feet of the acquired selected altitude. Altitude Select Bug Barometric Minimum Descent Altitude The Altitude Select Bug is displayed at the selected The desired barometric minimum descent altitude altitude or, if the selected altitude is beyond the altitudes (MDA, or Decision Height, DH) can be set in the Timer/ currently displayed, the bug is displayed at the top or References Window. bottom of the display (whichever is closest to the selected Visual annunciations alert the pilot when approaching altitude). the MDA: To set the Selected Altitude Bug: • When the aircraft altitude descends to within 2500 Turn the ALT Knobs to set the Altitude Select feet of the MDA setting, the Barometric Minimum Bug. The small ALT Knob sets the hundreds and Box appears with the altitude in light blue text. the large ALT Knob sets the thousands. This The bug appears on the tape in light blue once in altitude also appears in the Selected Altitude range. Box above the Altimeter. • When the aircraft passes through 100 feet of the MDA, the bug and text turn white. Altitude Trend Vector • Once the aircraft descends past the MDA, the bug The end of the trend vector displays approximately and text turn yellow and the aural alert, “Minimums what the altitude will be in 6 seconds if the current rate of Minimums”, is generated. vertical speed is maintained. Alerting is inhibited while the aircraft is on the ground. Barometric Setting Box If the aircraft climbs after having reached the MDA, once it reaches 50 feet above the MDA, alerting is disabled. To set barometric pressure, turn the BARO Knob to select the desired setting.

2-4 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 2 FLIGHT INSTRUMENTS

Within 2500 ft Within 100 ft 2.5 VERTICAL DEVIATION/GLIDESLOPE INDICATOR The Vertical Deviation/Glideslope Indicator appears when an ILS is tuned in the active NAV frequency ﬁeld. Barometric Mini- mum Bug 2.6 VERTICAL SPEED INDICATOR Barometric Minimum Box Selected Vertical Speed Altitude Reached

Vertical Speed Bug Vertical Speed Pointer

Figure 2-9 Barometric Minimum Descent Altitude Alerting Visual Annunciations

2.4 MARKER BEACON ANNUNCIATIONS Figure 2-11 Vertical Speed Indicator

Marker Beacon The actual vertical speed is displayed inside the Annunciation pointer. When the Flight Director is placed in Vertical Speed Mode (by pressing the VS Key) the Vertical Speed Bug is displayed. Press the NOSE UP or NOSE DN Key to Vertical Deviation/Glideslope adjust. Indicator 2.7 HORIZONTAL SITUATION INDICATOR (HSI) The HSI compass can be displayed as a 360° rose or Figure 2-10 Marker Beacon and Vertical Deviation 140° arc by pressing the PFD Softkey, followed by the 360 HSI or the ARC HSI Softkey.

Garmin G1000 Cockpit Reference Guide for the DA40 2-5 SECTION 2 FLIGHT INSTRUMENTS

14 13 Turn Rate Indicator and Heading Trend Vector Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta turn rate trend vector shows the current turn rate. The 1 12 end of the trend vector gives the heading predicted in six seconds, based on the present turn rate. At rates greater 2 11 than 4 deg/sec, an arrowhead appears at the end of the 3 10 magenta trend vector and the prediction is no longer valid. 4 9 Half-Standard Turn 8 Rate Tick Mark Turn Rate 5 Standard Turn Trend Vector Rate Tick Mark (rate > 4 7 deg/sec) 6

Figure 2-13 Turn Rate Indicator and Trend Vector 1 Turn Rate Indicator 2 Lateral Deviation Scale Turn Rate 3 Navigation Source Trend Vector (standard rate) 4 Aircraft Symbol 5 Course Deviation Indicator 6 Rotating Compass Rose Figure 2-14 Standard-Rate Turn Indication 7 OBS Mode Course Pointer 8 TO/FROM Indicator The Course Pointer is a single line arrow (GPS, VOR1 9 Heading Bug and LOC1) or double line arrow (VOR2 and LOC2) which 10 Course Pointer points in the direction of the set course. 11 Flight Phase 12 Turn Rate and Heading Trend Vector 13 Heading 14 Lubber Line

Figure 2-12 Horizontal Situation Indicator (360º) Lateral Deviation Course Deviation Scale TO/FROM Indicator

Figure 2-15 Arc CDI and Compass Rose CDI

2-6 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 2 FLIGHT INSTRUMENTS

Course Deviation Indicator (CDI) Distance to Bearing Source The CDI scale automatically adjusts to the current phase of flight (enroute 5.0 nm, terminal area 1.0 nm, Waypoint or approach 0.3 nm). Scaling may be selected manually Identifier from the MFD System Setup Page. See System Setup in Bearing Pointer the G1000 Pilot’s Guide for more details. Source Icon Figure 2-17 BRG1 Information Window Bearing Pointers and Information Windows Pressing the PFD Softkey provides access to the BRG1 Distance to Bearing Source and BRG2 Softkeys. The BRG1 Pointer is a single line pointer. The BRG2 Pointer is a double line pointer. Waypoint Identifier DME Information Bearing 1 Window Pointer Bearing 2 Pointer Bearing Pointer Icon Source Figure 2-18 BRG2 Information Window

DME (optional) To display the DME Information Window, press the PFD Softkey followed by the DME Softkey.

Bearing 1 Bearing 2 Figure 2-19 DME Information Window Information Information Window Window Figure 2-16 HSI with Bearing Information Navigation Source To change between navigation sources: 1) Press the CDI Softkey to change from GPS to VOR1/LOC1. 2) Press the CDI Softkey again to change from VOR1/LOC1 to VOR2/LOC2. 3) Press the CDI Softkey a third time to return to GPS.

Garmin G1000 Cockpit Reference Guide for the DA40 2-7 SECTION 2 FLIGHT INSTRUMENTS

When using GPS as the navigation source, the following may appear: NOTE: The OBS Softkey is only displayed when navigating an active leg using GPS. • INTEG – GPS information is either not present or is invalid for navigation use • WARN – GPS detects a position error . • SUSP – Displayed when in OBS Mode indicating GPS waypoint sequencing is suspended.

Figure 2-20 GPS INTEG, GPS SUSP, LOC1 and VOR2 To enable/disable OBS mode while navigating with GPS: 1) Press the OBS Softkey to select OBS Mode. 2) Turn the CRS Knob to select the desired course TO/FROM the waypoint. 3) Press the OBS Softkey again to return to normal operation.

2-8 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 3 – ENGINE INDICATION SYSTEM (EIS)

SECTION 3: ENGINE INDICATION SYSTEM (EIS) RPM Gauge

3.1 ENGINE DISPLAY Fuel Flow Indicator In all cases green indicates normal operation, yellow Cylinder Head indicates caution, and red indicates warning. Temperature Indicator Pressing the ENGINE Softkey makes available the Oil Temperature LEAN and SYSTEM Softkeys which in turn provide access Indicator to the Lean Display and the System Display, respectively. Oil Pressure Indicator

Manifold Ammeter Pressure Gauge Voltmeter

RPM Gauge Fuel Quantity Indicator

Figure 3-2 DA40F (Fixed Pitch Propeller) Fuel Flow Indicator Default Engine Display Cylinder Head Temperature Indicator Fuel Pressure Indicator (Option, DA40 only) Oil Temperature Indicator Located between the Fuel Flow and CHT Indicators Oil Pressure Indicator and shows the fuel pressure in pounds per square inch. • Green – Normal Ammeter • Red – Warning (minimum and maximum) Fuel Quantity Indicator (scale Voltmeter is 0 - 25 with extended range fuel tanks) Figure 3-3 Fuel Pressure Indicator Figure 3-1 DA40 Default Engine Display (Showing Warning)

Garmin G1000 Cockpit Reference Guide for the DA40 3-1 SECTION 3 – ENGINE INDICATION SYSTEM (EIS)

3.2 LEAN ENGINE DISPLAY

Cylinder Select Fuel Flow The CYL SLCT Softkey can be utilized to obtain Indicator information about a particular cylinder. The CYL SLCT Softkey becomes disabled when a particular cylinder turns yellow or red, until the temperature decreases and returns to normal or when the ASSIST Softkey is pressed. Exhaust Gas Temperature Bar Graph EGT Readout Temperature For Selected Deviation Cylinder From Peak

Cylinder Head Temperature CHT Readout Bar Graph Fuel Flow For Selected Indicator Cylinder Hollow Bar Figure 3-5 DA40F (Fixed Pitch Propeller) Exhaust Gas Representing Peak LEAN Engine Display Temperature Bar Graph EGT Readout Pressing the ASSIST Softkey causes the ﬁrst cylinder For Selected Temperature Cylinder Deviation EGT that peaks to become highlighted and information From Peak for that cylinder to be displayed. CHT Readout Cylinder Head For Selected Temperature Cylinder Bar Graph

Figure 3-4 DA40 LEAN Engine Display

3-2 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 3 – ENGINE INDICATION SYSTEM (EIS)

3.3 ENGINE SYSTEM DISPLAY

If desired, use the DEC FUEL, INC FUEL and RST FUEL Softkeys to adjust the amount of fuel remaining for totalizer calculations.

System NOTE: Fuel calculations do not use the aircraft Information fuel quantity indicators, and are calculated from the last time the fuel was reset.

Fuel Calculation Information

System Information Aircraft Total Fuel Pressure Time in Service Indicator is Optional on the Figure 3-7 DA40F (Fixed Pitch Propeller) DA40 SYSTEM Engine Display

Fuel Calculation Information

Aircraft Total Time in Service Figure 3-6 DA40 SYSTEM Engine Display

Garmin G1000 Cockpit Reference Guide for the DA40 3-3 SECTION 3 – ENGINE INDICATION SYSTEM (EIS)

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3-4 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 4 – NAV/COM & TRANSPONDER

SECTION 4: NAV/COM AND TRANSPONDER

The Nav/Com controls and frequency boxes are located on the Primary Flight Display and the Multi-Function Display in the same locations.

NAV COM Controls NAV Frequency Box COM Frequency Box Controls

Figure 4-1 G1000 VHF NAV/COM Interface (PFD)

Garmin G1000 Cockpit Reference Guide for the DA40 4-1 SECTION 4 – NAV/COM & TRANSPONDER

Standby NAV Selected NAV Selected COM Standby COM Frequency Field Frequency Frequency Frequency Field

Figure 4-2 Frequency Fields Tuning Box Active NAV Active COM Tuning Box Frequency Field Frequency Field

Frequency Toggle Arrow Tuning Box

Figure 4-3 Frequency Toggle Arrow and Tuning Box

NAV Controls COM Controls

VOL/PUSH VOL/PUSH ID Knob SQ Knob Frequency Toggle Key

Dual NAV Dual COM Knob Knob

• Turn to tune in desired frequencies. • Press to change tuning box positions. Figure 4-4 NAV/COM Controls

4-2 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 4 – NAV/COM & TRANSPONDER

4.1 RADIO STATUS INDICATIONS for approximately two (2) seconds automatically tunes the selected COM radio to the emergency frequency. • RX – When a COM signal is received, a white ‘RX’ appears by the active COM frequency during signal 4.5 OPTIONAL NAV RADIOS reception. The ADF/DME Tuning Window is displayed by • TX – When a COM radio is transmitting, a white ‘TX’ pressing the ADF/DME Softkey (if no ADF is installed, indication appears to the right of the corresponding the softkey will be labeled DME). COM frequency. ADF Radio (optional) • ID – When the Morse code identifier is ON for a NAV radio, a white ‘ID’ indication appears to the left of To tune the ADF: the corresponding active NAV frequency. The Morse 1) From the tuning window, turn the large FMS code identifier can be heard if the corresponding Knob to highlight the ADF tuning field. NAV radio is selected on the audio panel. 2) Turn the small FMS Knob to enter the first digit. 3) Turn the large FMS Knob to select the next Figure 4-5 Radio Status Indications desired digit field. Turn the small FMS Knob 4.2 VOLUME to again select the desired digit. 4) When the desired frequency is entered press ‘VOLUME’ is displayed in place of the associated radio the ENT Key to transfer the frequency into the name (i.e., ‘COM1’ or ‘NAV2’) for two seconds after the active field. volume level is last changed. The percentage of maximum 5) Turn the large FMS Knob to select the MODE volume is displayed in place of the standby frequency field. Turn the small FMS Knob to select ADF selected by the tuning box. or BFO. 6) Turn the large FMS Knob to select the volume field if desired. Turn the small FMS Knob to Figure 4-6 COM Volume Level adjust the ADF volume to the desired level. 4.3 AUTOMATIC SQUELCH 7) Press the FMS Knob to exit all the fields. Automatic squelch can be disabled for a COM radio by pressing the COM Knob to place the tuning box on the desired COM’s standby frequency, then by pressing the VOL/PUSH SQ Knob. 4.4 QUICKLY ACTIVATING 121.500 MHZ

Pressing and holding the COM Frequency Toggle Key Figure 4-7 ADF/DME Tuning Window

Garmin G1000 Cockpit Reference Guide for the DA40 4-3 SECTION 4 – NAV/COM & TRANSPONDER

DME Radio (optional) 4.6 FREQUENCY AUTO-TUNING Auto-tuning on the PFD

Figure 4-8 ADF/DME Tuning Window

To change the DME tuning source: 1) From the tuning window, turn the large FMS Figure 4-10 Nearest Airports Window (PFD) Knob to highlight the desired DME source. 1) Press the NRST Softkey to display the Nearest 2) Turn the small FMS Knob to display the Airports Window. selection window. Turn the FMS Knob to select 2) Turn the FMS Knobs to highlight the desired the desired mode and press the ENT Key. frequency. 3) Press the ENT Key to place the frequency in the standby field of the active COM. 4) Press the Frequency Toggle Key to place the frequency in the active field. NAV frequencies are entered automatically in the NAV Figure 4-9 DME Selection Window active frequency field upon approach loading or approach activation.

Auto-tuning on the MFD Auto-tuning on the MFD is done in much the same way as on the PFD. Use the FMS Knobs to select the desired frequency on any of the information pages. Pressing the ENT Key then loads the selected frequency in the tuning box as a standby frequency.

4-4 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 4 – NAV/COM & TRANSPONDER

4.7 TRANSPONDER Following is a list of important codes: • 1200 – VFR code in the U.S. (please refer to the Mode Selection ICAO standards for VFR codes in other countries). The STBY, ON and ALT Softkeys can be accessed by • 7000 – VFR code commonly used in Europe (please pressing the XPDR Softkey. refer to the ICAO standards). • 7500 – Hijack code. Ground Mode (Automatic) • 7600 – Loss of communication code. GND is displayed when the aircraft is on the ground. • 7700 – Emergency code. • 7777 – Military interceptor operations code (NEVER ENTER THIS CODE). • 0000 – Code for military use (in the U.S.). Figure 4-11 Ground Mode Flight ID Reporting Reply Status If so configured, the Flight ID may be entered in When the transponder sends replies to interrogations, the Timer/Reference Window. If configuration is set to an “R” indication appears momentarily in the reply status “SAME AS TAIL” the aircraft tail number will always be field. displayed.

Figure 4-12 Reply Indication

Code Selection 1) Press the XPDR Softkey to display the

transponder Mode Selection softkeys. Flight ID 2) Press the CODE Softkey to display the Figure 4-13 Timer/References Window transponder Code Selection softkeys, which includes the digit softkeys. 3) Press the appropriate digit softkeys to enter the code in the four-digit code ﬁeld of the Transponder Status Box. Five seconds after the fourth digit has been entered, the transponder code becomes activated. When entering a code, press the BKSP Softkey as needed to back up and change code digits.

Garmin G1000 Cockpit Reference Guide for the DA40 4-5 SECTION 4 – NAV/COM & TRANSPONDER

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4-6 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 5 – AUDIO PANEL

SECTION 5: AUDIO PANEL

Transmitters Transceiver Audio (COM3 MIC is unavailable) (COM 3 is unavailable)

Split COM (Unavailable) Telephone (Unavailable)

Passenger Address Speaker

Marker Beacon/Mute Marker Beacon Signal Sensitivity

Aircraft Navigation Radio Audio Aircraft Navigation Radio Audio (ADF & DME optional, AUX unavailable)

Manual Squelch Recorded COM Audio Playback

ICS Isolation

VOL/SQ Volume/Squelch VOL Annunciation SQ Annunciation Reversionary Mode

Figure 5-1 Audio Panel Controls

Garmin G1000 Cockpit Reference Guide for the DA40 5-1 SECTION 5 – AUDIO PANEL

5.1 COM RADIO SELECTION Marker Beacon Signal Sensitivity Pressing the COM1 MIC or COM2 MIC Key selects The HI SENS Key can be pressed for increased marker the active transmitter (i.e., microphone). The associated beacon signal sensitivity. receiver audio (COM1 or COM2) also becomes selected when the COM MIC Key is pressed. To prevent deselecting the desired received audio when pressing another COM MIC Key, press the already Figure 5-4 Marker Beacon selected COM1 or COM2 Key before pressing the other COM MIC Key. 5.3 NAV RADIO AUDIO SELECTION Pressing DME, ADF, NAV1, or NAV2 selects and deselects the radio source and activates the annunciator. Selected audio can be heard over the headset and the speakers. These four keys can be selected individually Figure 5-2 Transceivers or together.

5.2 MARKER BEACON RECEIVER The marker beacon receiver is always ON. Figure 5-3 shows the marker beacon annunciators on the PFD

Inner Marker Middle Marker Outer Marker Annunciator Annunciator Annunciator

Figure 5-3 Marker Beacon Signal Indicator Lights on the PFD

When the MKR/MUTE Key is pressed, the key annunciator is lit and the audio tone can be heard over the speaker or headsets during marker reception. When the tone is active, pressing the MKR/MUTE Key mutes the audio but does not affect the annunciator. The audio returns when the next marker signal is received.

5-2 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 5 – AUDIO PANEL

5.5 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ Key to light the annunciator. Pressing the small VOL/SQ Knob now toggles between Figure 5-5 Navigation Radios volume and squelch adjustment by lighting VOL or SQ respectively. 5.4 INTERCOM SYSTEM (ICS) ISOLATION Press the PILOT and/or COPLT Key to select who is isolated from hearing the Nav/Com radios and music. Selection scenarios are addressed in Table 5-1.

Figure 5-6 ICS Isolation

Figure 5-7 Volume/Squelch Control

PILOT KEY COPLT KEY Passenger Mode Pilot Hears Copilot Hears ANNUNCIATOR ANNUNCIATOR Hears Selected radios; Selected radios; Selected radios; pilot; copilot; pilot; copilot; pilot; copilot; ALL OFF OFF passengers; passengers; passengers; MUSIC 1 MUSIC 1 MUSIC 2 Copilot; Copilot; Selected radios; PILOT ON OFF passengers; passengers; pilot MUSIC 1 MUSIC 2

Selected radios; Selected radios; COPILOT OFF ON pilot; passengers; Copilot pilot; passengers; MUSIC 1 MUSIC 2

Selected radios; Selected radios; Passengers; CREW ON ON pilot; copilot pilot; copilot MUSIC 2

Table 5-1 ICS Isolation Modes

Garmin G1000 Cockpit Reference Guide for the DA40 5-3 SECTION 5 – AUDIO PANEL

5.6 DIGITAL CLEARANCE RECORDER AND PLAYER

Each reception of primary active COM audio is automatically recorded in a memory block. When the next transmission is received, it is recorded in the next memory block, and so on. Once the 2.5 minutes of recording time has been reached, the recorder begins recording over the stored memory blocks, starting from the oldest block. Powering off the unit automatically clears all recorded blocks.

Figure 5-8 Playback

• Pressing PLAY once plays the latest recorded memory block, then returns to normal operation. • Pressing PLAY again while playing a memory block halts playing of this block and plays the preceding recorded block. The PLAY Key can be used to move back through the recorded memory blocks to reach and play any desired block. • Pressing the MKR/MUTE Key during play halts playing and returns the recorder/playback to normal operation. If a COM input signal is detected during while playing, play is halted and the new COM input signal is recorded as the latest block.

5-4 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 6 – AUTOMATIC FLIGHT CONTROL

SECTION 6: AUTOMATIC FLIGHT also being active, ‘PTRM’ is displayed in the AFCS System Status Box on the PFD. Pressing the ARM CONTROL switch also acknowledges an autopilot disconnect. The GFC 700 AFCS is optional on the DA40 and DA40F. In aircraft without the GFC 700 option, refer to the operating instructions for the installed autopilot system for details. In addition to the AFCS (Automatic Flight Control System) keys on the MFD, as discussed in the System Overview section, the following buttons and switches used by the AFCS are located in the cockpit separately from the PFD and MFD. Figure 6-1 AFCS Keys • AP DISC (Autopilot Disconnect) Button — Located on the left and right control sticks, pressing Pressing the FD Key activates only the flight director this button disengages the autopilot. Pressing it also in the default Pitch Hold/Roll modes without engaging the acknowledges an autopilot disconnect. autopilot. Pressing the AP Key activates the flight director and engages the autopilot. When only the flight director is • CWS (Control Wheel Steering) Button — engaged, pressing the FD Key removes the flight director. Located on the left and right control sticks, pressing Upon activation of the autopilot and/or flight director, and holding the CWS button disengages the control command bars are displayed on the PFD. If the attitude surface servos without disengaging the autopilot. If information being sent to the flight director becomes the flight director has not been activated, pressing invalid or unavailable, the command bars are removed the CWS button will activate the flight director in from the display. the default pitch and roll hold modes. • GA (Go Around) Button — Located on the throttle lever, the GA button disengages the autopilot and selects the Go Around (wings level) mode. Figure 6-2 Command Bars • AP TRIM (Autopilot Trim) Switch — Located on 6.1 MODE ANNUNCIATIONS the left control stick, this switch is used to operate Mode annunciations are displayed on the PFD. Figure manual electric pitch trim. Moving both switches 6-3 shows the AFCS Status Box. Modes associated with forward simultaneously trims the aircraft nose down. aircraft movement about the roll axis are displayed on the Moving both switches aft simultaneously trims the left side. Modes associated with aircraft movement about aircraft nose up. The left switch is the ARM contact the pitch axis are displayed on the right. Armed modes and the right switch controls the up/down trim. are displayed in white and active modes are displayed in Pressing the ARM switch disengages the autopilot, if green. currently engaged. If one side of the switch is active for more than three seconds without the other side

Garmin G1000 Cockpit Reference Guide for the DA40 6-1 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Active Mode Mode Reference Armed Mode Autopilot Status Active Mode Armed Mode

Roll Axis Modes Pitch Axis Modes AFCS Status Box

System Status Annuciation Selected Altitude (see Annunciations & Alerts) Box Aircraft Attitude Symbol

Flight Director Command Bars

Figure 6-3 PFD AFCS Display 6.3 AP ENGAGEMENT/DISENGAGEMENT 6.2 OVERSPEED PROTECTION When the AP Key is pressed, the system engages the An overspeed annunciation (ﬂashing inverse video) is autopilot. If the ﬂight director is not already active, it is displayed above the airspeed tape. also engaged when the AP Key is pressed. Autopilot engagement is displayed in the Autopilot Status Field of the AFCS Status Box. Autopilot engagement is indicated by a green ‘AP’. Figure 6-4 Overspeed Annunciation

When an overspeed caution occurs, reduce engine Autopilot Engaged power and/or adjust the pitch reference to slow the aircraft. Figure 6-5 Autopilot Engaged Annunciation

6-2 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Automatic Disengagement 6.4 LOSS OF DATA Automatic disengagement typically occurs due to a In general, a flashing yellow mode annunciation failure. Automatic disengagement is annunciated by a indicates either the loss of sensor data (AHRS, ADC, flashing ‘AP’, alternating red on white and white on red in or GIA) or loss of navigation data (VOR, LOC, or GPS) the Autopilot Status Field. Also, the autopilot disconnect required to compute commands. aural alert will be heard. Both the annunciation and the When such a loss occurs, the system automatically aural alert will continue until acknowledged by pressing reverts to the default mode for the affected axis (wings the AP DISC button or the AP TRIM ARM switch. level ROL for roll axis, PIT for pitch axis). The flashing Automatic Disconnect annunciation stops when the pilot presses the affected mode button or selects another mode for the axis. If no Figure 6-6 Automatic Disconnect Annunciation pilot action is taken, the flashing annunciation stops after ten seconds. Manual Disengagement The autopilot may also be manually disengaged by Figure 6-9 Loss of VOR Signal pressing the AP DISC button, the GA button, the AP TRIM ARM switch, or by pressing the AP Key on the MFD. Manual disengagement is annunciated by a five- 6.5 PITCH AXIS MODES second flashing yellow ‘AP’ in the Autopilot Status Field Mode annunciations for active pitch axis modes are and by a two-second Autopilot disconnect aural alert. shown in green during normal operation. Note the Go- Manual Disconnect Around button is not located on the MFD. AFCS Key AFCS Mode Annunciation Figure 6-7 Manual Disconnect Annunciation FD/AP only Pitch Hold (Default) PIT Control Wheel Steering ALT Altitude Hold ALT nnnnn FT Pressing and holding the CWS button disengages the VS Vertical Speed VS nnnn FPM servos from the flight control surfaces and allows manual FLC Flight Level Change FLC nnn KT manuevering of the aircraft. At the same time, the flight APR Glideslope (vertical com- GS director is synchronized to the aircraft attitude during the ponent of Approach) maneuver. The ‘AP’ annunciation is temporarily replaced by ‘CWS’ in white until the CWS button is released. GA Go Around GA Control Wheel Steering The default pitch axis mode is Pitch Hold (PIT). When no other pitch axis modes are selected, this is the active pitch axis mode when the autopilot and/or flight director Figure 6-8 CWS Annunciation is engaged.

Garmin G1000 Cockpit Reference Guide for the DA40 6-3 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Pitch Hold Mode (PIT) selected altitude is reached ‘ALT’ will ﬂash in green for 10 seconds in the Acitve Mode Field, 1) Press the AP or FD Key. ‘PIT’ will be displayed after which the annunciation stops ﬂashing. in green in the Active Mode Field of the AFCS This signals the altitude capture is complete Status Box. The system will maintain or give and the selected altitude will be maintained. command bar direction for a constant pitch attitude (pitch reference) depending on which key is pressed. Pitch Hold mode is active Altitude Hold mode is armed

Flight Director command bars maintain desired pitch reference

Figure 6-10 Pitch Hold Mode 2) Altitude Hold mode is automatically armed with If only the ﬂight director is engaged, pitch and ‘ALT’ displayed white in the Armed Mode Field roll commands are given to manually maintain to the right of the ‘PIT’ annunciation. the selected altitude. 3) Pitch attitude can be adjusted in 0.5 degree increments by pressing the NOSE UP/NOSE DN Keys. 4) Aircraft pitch may also be changed by pressing and holding the CWS button to manually establish the desired pitch using the control stick. When the CWS button is released, the current pitch angle will be maintained. 5) If desired, enter an altitude in the Selected Altitude Box by turning the ALT Knob. As the

6-4 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Altitude Hold Mode (ALT) 3) To change aircraft altitude, press and hold the CWS button and manually maneuver 1) Press the ALT Key. The ﬂight director is activated to the desired altitude. Upon reaching the (if not already active) and ‘ALT’ is now displayed desired altitude, release the CWS button. This in green in the Active Mode Field with the new altitude is now displayed in the Altitude current altitude displayed in the Altitude Reference Field. The autopilot will now hold Reference Field. the aircraft at this altitude. 2) Pitch commands will be given to manually maintain the current altitude. Press the AP NOTE: If the Selected Altitude is captured during Key to engage the autopilot for maintaining CWS maneuvering, the Flight Director altitude the current altitude. reference is not changed. To adjust the altitude reference in this case, the pilot must again press the CWS button after the Selected Altitude is captured.

Altitude Hold mode is active Altitude Reference

Flight Director command bars hold pitch attitude to maintain the altitude reference

Figure 6-11 Altitude Hold Mode

Garmin G1000 Cockpit Reference Guide for the DA40 6-5 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Vertical Speed Mode (VS) The Vertical Speed Box is located above the VSI when the aircraft is climbing and below the VSI 1) Press the VS Key. The flight director is now when descending. activated (if not already active) and ‘VS’ is 3) Vertical speed may also be changed by pressing displayed in green in the Active Mode Field and holding the CWS button to manually and the Vertical Speed Bug will appear on the establish the desired vertical speed using the Vertical Speed Indicator. Pitch commands are control stick. When the CWS button is released, given to manually maintain vertical speed. the current vertical speed will be maintained. Press the AP Key to engage the autopilot for maintaining the current vertical speed. 4) A desired altitude may be entered in the Selected Altitude Box by turning the ALT Altitude Hold mode is automatically armed with Knob. With Altitude Hold mode armed, as the ‘ALT’ displayed white in the Armed Mode Field selected altitude is reached ‘ALT’ will flash in to the right of the ‘VS’ annunciation. green for 10 seconds in the Active Mode Field, 2) The Vertical Speed Bug can be adjusted in 100 after which the annunciation stops flashing. fpm increments by pressing the NOSE UP/NOSE This signals the altitude capture is complete DN Keys to set the desired vertical speed. The and the selected altitude will be maintained. vertical speed setting will be displayed in the If only the flight director is engaged, pitch and Selected Vertical Speed Box and in the Vertical roll commands are given to manually maintain Speed Reference Field in the AFCS Status the selected altitude. Box.

Vertical Speed Reference Vertical Speed mode is active Altitude Hold is Armed Selected Altitude Selected Vertical Speed Flight Director Vertical Speed command bars Reference Bug indicating a climb at the prescribed vertical speed, to the Selected Altitude

Figure 6-12 Vertical Speed Hold Mode

6-6 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Flight Level Change Mode (FLC) Airspeed Box above the Airspeed Indicator and in the Airspeed Reference Field in the AFCS 1) Select the desired altitude by turning the Status Box. ALT Knob to set the altitude in the Altitude Select Box. This altitude must be selected first 4) Airspeed may also be changed by pressing and because Flight Level Change mode will only fly holding the CWS button to manually establish toward a selected altitude. the desired airspeed using the control stick. When the CWS button is released, the current 2) Press the FLC Key. The flight director is airspeed will be maintained. activated (if not already active) and ‘FLC’ is now displayed in green in the Active Mode 5) Adjust engine power to allow the autopilot Field and the Airspeed Bug will appear on the to fly the aircraft at a pitch attitude which Airspeed Indicator. Pitch commands are given corresponds to the selected airspeed and the to manually maintain airspeed. Press the AP desired flight profile (descent or climb). Key to engage the autopilot for maintaining 6) With Altitude Hold mode armed, as the selected the current airspeed. altitude is reached, ‘ALT’ will flash in green Altitude Hold mode is automatically armed with for 10 seconds in the Acitve Mode Field, after ‘ALT’ displayed white in the Armed Mode Field which the annunciation stops flashing. This to the right of the ‘FLC’ annunciation. signals the altitude capture is complete and the selected altitude will be maintained. If only 3) The Airspeed Bug can be adjusted in 1 knot the flight director is engaged, pitch commands increments by pressing the NOSE UP/NOSE DN are given to manually maintain the selected Keys to set the desired airspeed. The airspeed altitude. setting will be displayed in the Selected Airspeed Reference Flight Level Change mode is active Altitude Hold mode is armed Selected Altitude Selected Airspeed

Airspeed Reference Bug

Figure 6-13 Flight Level Change Mode Garmin G1000 Cockpit Reference Guide for the DA40 6-7 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Go-Around Mode (GA) Glideslope (GS) Pressing the GA button (not located on the MFD) engages the ﬂight director in a wings level, 7 degree pitch NOTE: Pressing the CWS button while Glideslope up attitude. Go-Around mode disengages the autopilot, Mode is active does not cancel the mode. The and arms Altitude Hold Mode automatically. Subsequent autopilot guides the aircraft back to the glides- autopilot engagement is also allowed. If the pitch attitude lope upon release of the CWS button. is changed manually (e.g with the CWS button or the NOSE UP/NOSE DN Keys), Pitch and Roll Hold modes Glideslope Mode is only available when the ﬂight di- will automatically be selected. rector has been set for approach. Glideslope Mode is automatically armed under the following conditions: • Valid localizer frequency is tuned • Horizontal Situation Indicator (HSI) is in LOC mode, with valid deviation indication • Valid glideslope deviation • APR Key is pressed

Autopilot disconnect annunciation Go Around mode is ac- ﬂashes yellow for 5 seconds tive in both pitch axis & roll axis modes

Flight Director command bars indicating climb

Figure 6-14 Go-Around Mode

6-8 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 6 – AUTOMATIC FLIGHT CONTROL

6.6 ROLL AXIS MODES If the aircraft bank angle is < 6 degrees when the key is pressed, the aircraft will be Mode annunciations for active roll axis modes are maintained at wings level. If only the ﬂight shown in green during normal operation. director is active, command bars give guidance to maintain wings level. AFCS AFCS Mode Annunciation Key Roll Hold mode is annunciated by ‘ROL’. FD/AP only Roll Hold (Default) ROL

HDG Heading Select HDG Figure 6-15 Roll Hold Mode VOR Enroute VOR Arm / Capture / Track 2) A new heading can be established by pressing GPS Arm / Capture / Track GPS and holding the CWS button and manually NAV BC Arm / Capture / Track BC turning the aircraft to the desired new heading. Release the CWS button and the aircraft will LOC Arm / Capture / Track; LOC maintain wings level at approximately the new (No Glideslope) heading, but will not hold the heading. The GPS Arm / Capture / Track GPS same practice applies to holding roll attitude. VOR Approach VAPP Arm / Capture / Track APR ILS Approach Arm / Capture / Track LOC (Glideslope pitch mode automatically armed) GA Go Around (Wings Level) GA The default roll axis mode is Roll Hold (ROL). When no other roll axis modes are selected, this is the active roll axis mode when the autopilot and/or ﬂight director is engaged. Roll Hold Mode (ROL) 1) Press the FD or AP Key. If the aircraft bank angle is ≥ 6 degrees when the key is pressed, Roll Hold mode is selected by default. Roll attitude at the time of activation is maintained by the autopilot up to 22˚. If only the ﬂight director is active, command bars indicate the proper roll attitude. Garmin G1000 Cockpit Reference Guide for the DA40 6-9 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Heading Select Mode (HDG) 3) The heading may be adjusted by turning the HDG Knob and moving the heading bug to a 1) Turn the HDG Knob to move the heading bug new heading. The aircraft will turn in the same on the HSI to the desired heading. When the direction the heading bug is moved. However, knob is turned, the Selected Heading Box will if the heading bug is moved more than 340 appear and remain for three seconds after the degrees at a time, a turn reversal will be the knob stops moving. The selected heading will result. be displayed in the Selected Heading Box. 2) With the autopilot and/or flight director engaged, press the HDG Key. ‘HDG’ is now displayed in green in the Active Mode Field. If the autopilot is engaged, the aircraft will begin to turn toward the selected heading. When the selected heading is reached, the aircraft will maintain this heading. If only the ﬂight director is engaged, manually maneuver the aircraft to the command bars to aquire the selected heading.

Heading Select mode Altitude Hold mode is active

Flight Director command bars tracking Selected Heading

Selected Heading Box Selected Heading Bug

Figure 6-16 Heading Select Mode

6-10 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Navigation Mode (GPS, VOR, LOC, or BC) Navigation Mode Armed Pressing the NAV Key activates the Navigation Mode. If the CDI is not centered (deviation >1 dot) when the The Navigation mode acquires and tracks the selected Navigation mode is selected, the mode is automatically navigation receiver on the HSI (e.g. GPS, VOR or LOC). armed. The armed annunciation appears in white to the GPS roll steering commands are followed when the HSI left of the active roll axis mode. is in GPS mode, and creates roll steering commands from See the Example Procedures Using AFCS section for the Selected Course and deviation when the HSI is in more information. VOR, LOC, or BC (backcourse) modes. Turning the CRS Knob moves the Course Pointer and displays the Selected Course Box. The Selected Course is displayed in the box. The box is displayed while the knob is turning and disappears three seconds after the knob stops turning. Backcourse mode is automatically selected when the localizer front course is greater than 105 degrees from the aircraft heading.

NOTE: When making a backcourse approach, set Selected Course to the localizer front course.

Flight Level Change mode is active Navigation Mode is active using GPS source Altitude Hold is armed

Flight Director command bars indicating a left turn to track GPS course and a climb to intercept Selected Altitude Selected Course GPS is active navigation receiver on the HSI.

Figure 6-17 Navigation Mode

Garmin G1000 Cockpit Reference Guide for the DA40 6-11 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Approach Mode (GPS, VAPP or LOC) If the CDI is not centered (deviation >1 dot) when the Approach mode is selected, the mode is automatically The Approach mode acquires and tracks the selected armed. The armed annunciation appears in white to the navigation receiver on the HSI (GPS, VOR or LOC). This left of the active roll axis mode. mode uses the selected navigation receiver deviation and desired course inputs to ﬂy the approach. The Approach See the Example Procedures Using AFCS section for mode provides greater sensitivity for VOR tracking than more information. Navigation mode, and allows the autopilot to ﬂy an ILS approach with a glideslope. Go Around (GA)

NOTE: While using Approach mode, the Go Around mode maintains a wings level, 7 degree Glideslope mode is automatically armed when nose up attitude for instances where the pilot wishes to LOC mode is selected on the HSI. execute a missed approach or go around. Figure 6-14 depicts the Go Around mode on the PFD.

Approach Mode is active Glideslope is active

Flight Director command bars indicating descent on localizer/ glideslope path

LOC2 is the active navigation receiver on the HSI

Figure 6-18 Approach Mode

6-12 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 6 – AUTOMATIC FLIGHT CONTROL

6.7 EXAMPLE PROCEDURES USING AFCS NOTE: The diagrams in the following examples This section provides a scenario-based set of procedures are for instructional purposes only and may not showing various autopilot modes used during a flight. In be used for navigation. this scenario, the aircraft departs Reid-Hillview Airport (KRHV) from runway 13L, enroute to Fresno Yosemite International Airport (KFAT). Climb to an altitude of 7,000 feet MSL and fly a heading of 070 degrees to intercept airway V107. Fly airway V107 to Panoche VORTAC (PXN) using VOR navigation, then fly airway V230 using a GPS flight plan. Prior to reaching Clovis VORTAC (CZQ), descend to 3,000 feet and load the ILS approach to R29R at KFAT. Fly the ILS approach and execute a missed approach.

KRHV

070

V 33 0 1 07 0 3 3

Clovis� 3 0 3 6 7 2 VORTAC

0 3 (CZQ)

3 9

30 4

V 2 2 6 7

1 2

Panoche� 2

1 5 8

2 VORTAC 1

(PXN)

1 2

1 5 8 1

KFAT Figure 6-19 Flight Plan Overview

Garmin G1000 Cockpit Reference Guide for the DA40 6-13 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Departure 3) Activate Heading Select Mode while the autopilot is engaged in the climb. To climb to the selected altitude and fly an a) Use the HDG Knob to set the Selected Heading assigned heading: to 070°. 1) Upon takeoff, set the Selected Altitude to 7000 b) Press the HDG Key. The autopilot follows the feet using the ALT Knob. Heading Bug on the HSI and turns the aircraft To have the autopilot capture this altitude, use to the desired heading. Pitch Hold, Vertical Speed, or Flight Level Change Mode. In this example, Vertical Speed Mode is used. 4) As the aircraft climbs to the Selected Altitude, 2) Upon reaching the desired vertical speed of 1000 the flight director changes from Vertical Speed to fpm, enable the flight director in Vertical Speed Altitude Hold Mode. This active mode change is Mode. indicated by the green ‘ALT’ annunciation flashing a) Press the VS Key. Altitude Hold Mode is armed for ten seconds. automatically. 5) Upon reaching the Selected Altitude, the autopilot b) Press the AP Key to engage the autopilot in completes the capture process and levels the Roll Hold and Vertical Speed modes. aircraft. From this point, the flight director continues to operate in Altitude Hold Mode.

070 HDG Mode 3.

Selected Altitude of 7,000 MSL 5.ALT Mode 4. ed Arm de Mo ALT de, Mo 2. VS 1. Figure 6-20 Departure

6-14 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Intercepting a VOR Radial c) Press the NAV Key to arm Navigation Mode. The white annunciation ‘VOR’ appears to NOTE: Changing the HSI mode cancels the left of the active roll mode. Navigation Mode and causes the flight director to revert to Roll Hold Mode. 2) When the CDI shows less than one dot, the During climb-out, the autopilot continues to fly the flight director changes from Heading Select to aircraft in Heading Select Mode. Airway V107 to Panoche Navigation Mode, and the green annunciation VORTAC (PXN) should now be intercepted. ‘VOR’ flashes. The autopilot begins turning to intercept the Selected Course. 1) Tune the VOR frequency and activate Heading Select Mode. a) Use the CDI Softkey to set the HSI mode to 3) The autopilot continues the turn until the aircraft VOR. is established on the Selected Course. b) Use the CRS Knob to set the Selected Course to 116°. Note that at this point, the flight director is still in Heading Select Mode and the autopilot continues to fly 070°.

V 1 07

070 e, VOR Armed HDG Mod 2. V O 1. R 3. M o de

33 0 2 96 0 3 3

6 7

Panoche�

9 4

2 VORTAC�

(PXN)

1 2

1 5 8 1

Figure 6-21 Intercepting a VOR

Garmin G1000 Cockpit Reference Guide for the DA40 6-15 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Flying a GPS Flight Plan If the NAV Key is not pressed within 10 seconds of the HSI mode change, the flight 1) Enter Panoche VORTAC (PXN) and Clovis VORTAC director will roll the wings level and enter Roll (CZQ) into the GPS flight plan, in preparation to Hold Mode. intercept this leg. 3) Once the flight plan leg is intercepted, the 2) Transition from VOR to GPS Navigation Mode. autopilot continues to track GPS guidance to the a) Use the CDI Softkey to put the HSI in GPS end of the flight plan. mode. This cancels VOR mode on the HSI and the flight director loses the VOR signal. As a result, the VOR annunciation flashes yellow. Flashes for ten seconds, then transitions to ROL..

b) Press the NAV Key to activate GPS Navigation Mode to cause the autopilot to steer the aircraft toward the active ﬂight plan leg.

33 0

0 3 3 1. V O R

6 M 7 o 2 de 2. 33 0

0 3 Clovis�

3 9 4

2 VORTAC (CZQ) G PS 0

Mo V 23 6

7 d

e 3. 1

2 1 2

Leg 2

Plan

light 1 F 5 8 PS 1

Panoche� G

VORTAC 9 4

2 (PXN)

1 2

1 5 8 1

Figure 6-22 Transition to GPS Flight Plan

6-16 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Flight Level Change (Descent) 2) Reduce power to allow descent in Flight Level Change Mode. The autopilot maintains the While flying the GPS leg from Panoche VORTAC to Airspeed Reference. Clovis VORTAC, the aircraft is cleared to make a descent to 3000 feet in preparation for the approach to KFAT. 3) Upon capturing the Selected Altitude, the flight director changes from Flight Level Change to 1) Enter Flight Level Change Mode. Altitude Hold Mode. The annunciation ‘ALT’ a) Using the ALT Knob, set the Selected Altitude flashes in green to indicate the altitude capture. to 3000 feet. After the capture is complete, the autopilot holds b) Press the FLC Key to activate Flight Level the aircraft level at the Selected Altitude. Change Mode. The annunciation ‘FLC’ appears next to the Airspeed Reference, which defaults to the current aircraft airspeed, 142 knots. Altitude Hold Mode is armed automatically.

1. Cruise Altitude of 7,000 MSL 2.

F LC M ode

3. Selected Altitude of 3,000 MSL ALT Hold Mode

Figure 6-23 FLC Descent

Garmin G1000 Cockpit Reference Guide for the DA40 6-17 SECTION 6 – AUTOMATIC FLIGHT CONTROL

ILS Approach 3) In preparation for approach, tune the localizer frequency and select LOC mode on the HSI. 1) Transition from GPS Navigation Mode to Heading 4) Press the APR Key when cleared for approach Select Mode. to arm the Approach Mode. ‘LOC’ and ‘GS’ a) Load the Runway 29R ILS approach for KFAT appear in the armed roll and pitch mode fields, into the Flight Plan. respectively. b) Select ‘Vectors to Final’ for the transition. The autopilot and flight director determine when c) Set the Selected Heading after getting vectors to begin the turn to intercept the final approach from ATC and press the HDG Key. The autopilot course. turns the aircraft to the desired heading. 5) The autopilot flies the ILS Approach. At the 2) Use Heading Select Mode to comply with ATC Decision Height, there are two options: push the vectors as requested. AP DISC switch and land the aircraft, or use the GA button to execute a missed approach (refer to 3 0 3 the following procedure). 3 30

Clovis 6

272

(CZQ)

9 9

4 e 4

2 24

GPS Cours 24

12 12

21 21

1. 21

15 15 5 8 18 18

29 0 12 2 KFAT

HDG Mode

LOC/GS Mode 5. 5 02 HILAN

11 4. 0 2. 075 3. Figure 6-24 ILS Approach to KFAT

6-18 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Go-Around / Missed Approach 4) To use the autopilot to fly the hold in Heading Select Mode, set the Selected Heading using the 1) Push the GA button at the Decision Height and HDG Knob and press the HDG Key. Use the HDG apply full power to execute a missed approach. Knob guide the aircraft for the remainder of the The flight director Command Bars establish a hold. nose-up climb to follow. Note that when the GA button is pushed, the autopilot disconnects and the ‘AP’ annunciation flashes yellow for five seconds Flashes for five seconds

2) Start the climb to the prescribed altitude in the 33 0

published Missed Approach Procedure. 3 HDG Mode30

a) Press the AP Key to re-engage the autopilot. 127

6 7 2 Clovis b) Set the HSI to GPS mode. VORTAC

c) Press the NAV Key to have the autopilot ﬂy to 4. CZQ

9 4

the hold. 2

5 8 d) Select the SUSP Softkey to resume sequencing 1

approach legs to the Missed Approach Hold GPS Mode Point (MAHP). The autopilot flies direct to Clovis VORTAC according to the loaded approach (see Figure 6-25). 3) Use the ALT Knob to set a Selected Altitude to hold. The CWS button may be used to set a new 3. pitch attitude. 2. As the Selected Altitude is captured, Altitude KFAT GA Mode 1. Hold Mode becomes active and the autopilot maintains the Selected Altitude. Figure 6-25 Go Around / Missed Approach

Garmin G1000 Cockpit Reference Guide for the DA40 6-19 SECTION 6 – AUTOMATIC FLIGHT CONTROL

Blank Page

6-20 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 7 – NAVIGATION

SECTION 7: NAVIGATION 7.2 DIRECT-TO NAVIGATION The following discussions pertain to the Multi Function Direct-to Navigation from the MFD Display, unless otherwise indicated. Identiﬁer Symbol Facility Name 7.1 NAVIGATION MAP PAGE City Flight Plan Field Nearest Airport Select the MAP Page Group Map Orientation 1) Turn the large FMS Knob until ‘MAP’ is Map of the Selected highlighted in the Page Group Box in the lower Waypoint right of the MFD display. Map Range 2) Turn the small FMS Knob to select the ﬁrst MAP Bearing Region page (indicated by a solid rectangular icon). Distance Latitude/ Longitude 3) Press the MAP Softkey to display softkeys Direct-to Activate Field for the available information which may be Course displayed on the map. Figure 7-2 MFD Direct-to Window

WARNING: The map display should only be Enter a Direct-to Destination used for situational awareness. Any map display indication should be compared with approved 1) Press the Direct-to ( ) Key. navigation sources. 2) Turn the small FMS Knob to enter the first letter of the destination waypoint identifier. Turn the large FMS Knob to the right to move the cursor to the next character position. 3) Repeat step 2 to spell out the rest of the waypoint identifier. 4) Press the ENT Key to confirm the identifier. The ‘Activate?’ field is highlighted. 5) Press the ENT Key to activate. Select a Direct-to Destination to a Flight Plan Waypoint or Nearest Airport 1) While navigating an active flight plan, press the Direct-to ( ) Key. 2) Turn the large FMS Knob to highlight the ‘FPL/ Figure 7-1 Navigation Map Page NRST WAYPOINT’ field.

Garmin G1000 Cockpit Reference Guide for the DA40 7-1 SECTION 7 – NAVIGATION

3) Turn the small FMS Knob to display a list of waypoints or airports. 4) Continue turning the small FMS Knob to scroll through the list and highlight the desired waypoint or airport. Figure 7-3 Canceling Direct-to Navigation 5) Press the ENT Key to confirm the selection. Direct-to Navigation from the PFD Press ENT again to activate a Direct-to. WPT Symbol To Re-center the CDI to the Destination Waypoint Identifier WPT Location Press the Direct-to ( ) Key, followed Facility Name by pressing the ENT Key twice. If a missed Flight Plan WPT Nearest WPT Bearing to WPT Lat/Lon approach point (MAP) is the current destination, Distance from WPT the approach will be canceled. Course to Selected WPT To Manually Define the Direct-to Course Figure 7-4 PFD Direct-to Window 1) Press the Direct-to ( ) Key and enter a 1) Press the Direct-to Key ( ). waypoint as discussed in previous steps, or to 2) Turn the large FMS Knob to place the cursor in edit the active direct-to. the desired selection field. 2) Turn the large FMS Knob to highlight the 3) Turn the small FMS Knob to begin selecting the ‘COURSE’ field. desired identifier, location, etc. 3) Turn the FMS Knobs to select the desired course 4) Press the ENT Key. and press the ENT Key. 5) The cursor is now flashing on ‘ACTIVATE?’. 4) Press the ENT Key again to begin navigation Press the ENT Key again to activate. using the selected destination and course. Cancelling Direct-to Navigation Canceling Direct-to Navigation 1) Press the Direct-to ( ) Key. 1) Press the Direct-to ( ) Key. 2) Press the MENU Key to display the Options 2) Press the MENU Key to display the Direct-to Window. The cursor will be flashing on ‘Cancel options menu. Direct-to NAV’. 3) With ‘Cancel Direct-To NAV’ highlighted, press 3) Press the ENT Key to cancel the direct-to. the ENT Key. If a flight plan is still active, the G1000 resumes navigating the flight plan along the closest leg.

7-2 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 7 – NAVIGATION

7.3 AIRPORT INFORMATION a list is displayed from which to choose the desired location. 6) To remove the flashing cursor, press the FMS Knob. Access Runway Information 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to place the cursor on the ‘RUNWAYS’ identifier field. 3) Turn the small FMS Knob to display the next runway for the selected airport. Continue turning the small FMS Knob to select the desired runway. 4) To remove the flashing cursor, press the FMS Figure 7-5 Airport Information Page Knob. Access Frequency Information Select the Airport Information Page 1) With the Airport Information Page displayed, 1) Turn the large FMS Knob to select the ‘WPT’ press the FMS Knob to activate the cursor. page group. 2) Turn the large FMS Knob to move the cursor to 2) Turn the small FMS Knob to select the first the Frequencies Box. rectangular page icon. 3) Turn either FMS Knob to scroll through the list, Enter a Waypoint Facility Name or City Location placing the cursor on the desired frequency. If 1) With the Airport Information Page displayed, a listed frequency has sector or altitude restric- press the FMS Knob to activate the cursor. tions, the frequency is preceded by an info (‘i’) designation. Press the ENT Key to view the 2) Turn the large FMS Knob to select the facility information. The following may be displayed name or location (city) field. with the frequency: 3) Turn the small FMS Knob to select the desired • ‘TX’ – transmit only first character. • ‘RX’ – receive only 4) Turn the large FMS Knob to select the next • ‘PT’ – part time frequency character field. 4) Press the ENT Key to place the selected fre- 5) Repeat steps 3 and 4 until the facility name or quency in the standby field of the COM or NAV location is selected, then press the ENT Key. Frequency Box. If there are duplicate names in the database, 5) To remove the cursor, press the FMS Knob.

Garmin G1000 Cockpit Reference Guide for the DA40 7-3 SECTION 7 – NAVIGATION

7.4 INTERSECTION INFORMATION 7.5 NDB INFORMATION

Select the Intersection Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the second rectangular page icon.

Figure 7-7 NDB Information Page

Select the NDB Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the third Figure 7-6 Intersection Information Page rectangular page icon View Information on a Specific NDB Access Information on an Intersection 1) With the NDB Information Page displayed, 1) With the Intersection Information Page press the FMS Knob to activate the cursor. displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to highlight the desired selection field (identifier, name or 2) Turn the FMS Knobs to enter a name for the closest city). identifier and press the ENT Key. 3) Turn the FMS Knobs to enter an identifier, name 3) Press the FMS Knob to remove the flashing or city and press the ENT Key. cursor. 4) Press the FMS Knob to remove the flashing cursor.

7-4 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 7 – NAVIGATION

7.6 VOR INFORMATION 7.7 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on creating and modifying user deﬁned waypoints. 7.8 NEAREST AIRPORTS

Figure 7-8 VOR Information Page Select the VOR Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the fourth Figure 7-9 Nearest Airports Page rectangular page icon. Nearest Airport Information on the MFD Access Information on a VOR Select the Nearest Airports Page 1) With the VOR Information Page displayed, press the FMS Knob to activate the cursor. 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the large FMS Knob to highlight the desired selection field (identifier, name or 2) Turn the small FMS Knob to select the first closest city). rectangular page icon. 3) Turn the FMS Knobs to enter an identifier, name Access Information on a Specific Airport or city and press the ENT Key. 1) With the Nearest Airports Page displayed, 4) The ‘FREQUENCY’ field is now highlighted. press the APT Softkey to place the cursor in the If desired, press the ENT Key to place the ‘NEAREST AIRPORTS’ field. The first airport in frequency in the NAV receiver standby field. the nearest airports list is highlighted. 5) Press the FMS Knob to remove the flashing 2) Press the FMS Knob, then turn the large FMS cursor. Knob to highlight the desired airport. Garmin G1000 Cockpit Reference Guide for the DA40 7-5 SECTION 7 – NAVIGATION

3) Press the FMS Knob to remove the flashing Nearest Airports Information on the PFD cursor. Bearing TO Distance Access Runway Information for the Selected Airport Airport Symbol 1) With the Nearest Airports Page displayed, press Identifier the RNWY Softkey to place the cursor in the Runway Length ‘RUNWAYS’ field. 2) Turn the small FMS Knob to select the desired runway. 3) Press the FMS Knob to remove the flashing cursor. Primary COM Frequency Quickly Tune the COM Transceiver to a Nearby Figure 7-10 Nearest Airports Window Airport Frequency Press the NRST Softkey to display the PFD 1) With the Nearest Airports Page displayed, press Nearest Airports Window. the FREQ Softkey to place the cursor in the ‘FREQUENCIES’ field. View Information on a Specific Airport in the List 2) Turn either FMS Knob to select the desired 1) With the Nearest Airports Window displayed, frequency. turn either FMS Knob to place the cursor on 3) Press the ENT Key. The selected frequency is the desired airport identifier. placed in the COM standby frequency tuning 2) Press the ENT Key to display airport field. information. 4) Press the Frequency Transfer Key to place the 3) Press the ENT Key again (cursor is on ‘BACK’) frequency in the active field. to return to the list. 5) Press the FMS Knob to remove the flashing Load an Airport COM Frequency into the Active COM cursor. 1) With the Nearest Airports Window displayed, turn either FMS Knob to place the cursor on the desired airport frequency. 2) Press the ENT Key and the selected frequency will be placed in the COM standby frequency field. 3) Press the Frequency Transfer Key to make the frequency the active frequency.

7-6 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 7 – NAVIGATION

7.9 NEAREST INTERSECTIONS 7.10 NEAREST NDB

Figure 7-11 Nearest Intersections Page Figure 7-12 Nearest NDB Page

Select the Nearest Intersections Page Select the Nearest NDB Page

1) Turn the large FMS Knob to select the ‘NRST’ 1) Turn the large FMS Knob to select the ‘NRST’ page group. page group. 2) Turn the small FMS Knob to select the second 2) Turn the small FMS Knob to select the third rectangular page icon. rectangular page icon. View Information on the Nearest Intersection Access Information on a Specific NDB 1) With the Nearest Intersections Page displayed, 1) With the Nearest NDB Page displayed, press press the FMS Knob to activate the cursor. the FMS Knob to activate the cursor. 2) Turn either FMS Knob to select the desired 2) Turn either FMS Knob to select the desired NDB. intersection. The remaining information on the Nearest NDB 3) Press the FMS Knob to remove the flashing Page pertains to the selected NDB. cursor. 3) Press the FMS Knob to remove the flashing cursor.

Garmin G1000 Cockpit Reference Guide for the DA40 7-7 SECTION 7 – NAVIGATION

7.11 NEAREST VOR 2) Press the ENT Key. The selected VOR frequency is placed in the NAV standby frequency ﬁeld. Select the Nearest VOR Page 3) Press the FMS Knob to remove the ﬂashing 1) Turn the large FMS Knob to select the ‘NRST’ cursor. page group. 7.12 NEAREST USER WAYPOINT 2) Turn the small FMS Knob to select the fourth rectangular page icon.

Figure 7-14 Nearest User Waypoints Page Select the Nearest User Waypoint Page Figure 7-13 Nearest VOR Page 1) Turn the large FMS Knob to select the ‘NRST’ View Information on the Nearest VOR page group. 1) With the Nearest VOR Page displayed, press 2) Turn the small FMS Knob to select the fifth the VOR Softkey to place the cursor in the rectangular page icon. ‘NEAREST VOR’ Box. Select a Nearest User Waypoint 2) Turn either FMS Knob to select a VOR. 1) With the Nearest User Waypoint Page displayed, 3) Press the FMS Knob to remove the flashing press the FMS Knob to activate the cursor. If cursor. any previously entered User Waypoints are within 200 nm, these will be displayed with Select and Load a VOR Frequency the closest listed first. 1) With the Nearest VOR Page displayed, press the 2) Turn either FMS Knob to select the desired FREQ Softkey to highlight the VOR frequency waypoint. The remaining information on the in the ‘FREQUENCY’ field. Nearest User Waypoint Page pertains to the selected Nearest User Waypoint.

7-8 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 7 – NAVIGATION

3) Press the FMS Knob to remove the ﬂashing 7.14 NEAREST AIRSPACES cursor. 7.13 NEAREST FREQUENCIES

Figure 7-16 Nearest Airspaces Page Select the Nearest Airspaces Page Figure 7-15 Nearest Frequencies Page 1) Turn the large FMS Knob to select the ‘NRST’ Select the Nearest Frequencies Page page group. 2) Turn the small FMS Knob to select the seventh 1) Turn the large FMS Knob to select the ‘NRST’ rectangular page icon. page group. 2) Turn the small FMS Knob to select the sixth Airspace Alerts Box rectangular page icon. • If the projected course takes the aircraft inside an airspace within the next ten minutes, ‘Ahead’ is Select and Load the Nearest ARTCC, FSS, or Weather displayed. Frequency • If the aircraft is within two nautical miles of an 1) With the Nearest Frequencies Page displayed, airspace and the current course takes the aircraft press the ARTCC, FSS, or Wx Softkey to place inside, ‘Ahead < 2 nm’ is displayed. the cursor in the appropriate ﬁeld. • If the aircraft is within two nautical miles of an 2) Turn the FMS Knobs to select the desired facility airspace and the current course will not take the or frequency. aircraft inside, ‘Within 2 nm’ is displayed. • If the aircraft has entered an airspace, ‘Inside’ is 3) Press the ENT Key to load the frequency into displayed. the COM frequency standby ﬁeld.

4) Press the FMS Knob to remove the ﬂashing cursor. Garmin G1000 Cockpit Reference Guide for the DA40 7-9 SECTION 7 – NAVIGATION

View Additional Details for a Listed Airspace 1) With the Nearest Airspace Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to scroll through the list, highlighting the desired airspace. 3) Press the ALERTS Softkey to place the cursor in the ‘AIRSPACE ALERTS’ field. 4) Turn either FMS Knob to select the desired airspace. 5) Press the FMS Knob to remove the flashing cursor. View and Quickly Load the Frequency for a Controlling Agency 1) With the Nearest Airspace Page displayed, press the FREQ Softkey to place the cursor in ‘FREQUENCIES’ field. 2) Turn either FMS Knob to select the desired frequency. 3) Press the ENT Key to load the frequency into the COM frequency standby field. 4) Press the FMS Knob to remove the flashing cursor.

7-10 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 8 – FLIGHT PLANNING

SECTION 8: FLIGHT PLANNING 4) Repeat steps 2 and 3 until the desired name is entered. The following discussions pertain to the Multi Function 5) Press the ENT Key. Display, unless otherwise indicated. 6) Press the ENT Key a again to accept the new 8.1 USER DEFINED WAYPOINTS waypoint identifier. 7) The cursor is now in the ‘REFERENCE WAYPOINTS’ field. If desired, the waypoint can be defined by a reference waypoint. Turn the FMS Knobs to enter the position coordinates or the radial and distance from the reference waypoint. 8) Press the FMS Knob to remove the flashing cursor. Modify a User Waypoint 1) With the User Waypoint Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to move the cursor to Figure 8-1 User WPT Information Page the desired field and turn the small FMS Knob to make changes. Select the User WPT Information Page 3) Press the ENT Key to accept the changes. 1) Turn the large FMS Knob to select the ‘WPT’ 4) Press the FMS Knob to remove the flashing page group. cursor. 2) Turn the small FMS Knob to select the fifth Delete a User Waypoint rectangular page icon. 1) Select the User Waypoint Information Page Create a New User Waypoint and press MENU to display the User Waypoint Information Page Options or press the DELETE 1) With the User Waypoint Information Page Softkey. displayed, press the NEW Softkey. A waypoint 2) Turn the large FMS Knob to select ‘Delete User is created at the current aircraft position. Waypoint’ and press the ENT Key. The message 2) Turn the small FMS Knob to enter first character ‘Would you like to delete the user waypoint’ of the waypoint name. is displayed. With ‘YES’ highlighted, press the 3) Turn the large FMS Knob to move the cursor to ENT Key. the next character field.

Garmin G1000 Cockpit Reference Guide for the DA40 8-1 SECTION 8 – FLIGHT PLANNING

Create User Waypoints from the Navigation Map Page 1) With the Navigation Map Page displayed, push the Joystick to activate the panning function. The map pointer is displayed at the present aircraft position. 2) Move the Joystick to place the pointer at the desired position 3) Press the ENT Key. The User Waypoint Information Page is now displayed with the captured position. 4) Turn the FMS Knobs to select a waypoint Figure 8-3 Active Flight Plan Window on the MFD name. 5) Press the ENT Key to accept the selected 8.3 ACTIVATE A STORED FLIGHT PLAN name. The first reference waypoint field is 1) Press the FPL Key and turn the small FMS Knob highlighted. to display the Flight Plan Catalog Page. 6) If desired, turn the FMS Knobs to enter the identifier of the reference waypoint and the radial and distance to the reference waypoint. Press the ENT Key to accept. 7) Press the FMS Knob to remove the flashing cursor. 8.2 VIEWING THE ACTIVE FLIGHT PLAN Press the FPL Key.

Figure 8-4 Flight Plan Catalog Page 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired Figure 8-2 Active Flight Plan Window on the PFD flight plan and press the ACTIVE Softkey. 4) With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.

8-2 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 8 – FLIGHT PLANNING

8.4 ACTIVATE A FLIGHT PLAN LEG the flight plan. This will not delete the stored flight plan, only the active flight plan. 1) From the Active Flight Plan Page, press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired destination waypoint. Figure 8-7 Delete Flight Plan Confirmation 2) Press the ACT LEG Softkey (using MFD only). OR 8.6 INVERT ACTIVE FLIGHT PLAN 3) Press the MENU Key, select the ‘Activate Leg’ 1) From the Active Flight Plan Page, press the option from the page menu and press the ENT MENU Key to display the Page Menu. Key. This step must be used when activating a leg from the PFD. 2) Turn the large FMS Knob to highlight ‘Invert Flight Plan’ and press the ENT Key. The original 4) With ‘Activate’ highlighted, press the ENT flight plan remains intact in its flight plan Key. catalog storage location. 3) With ‘OK’ highlighted, press the ENT Key to invert the flight plan.

Figure 8-5 Activate Flight Plan Leg Conﬁrmation

8.5 STOP NAVIGATING A FLIGHT PLAN 1) Press the FPL Key to display the Active Flight Plan Page. 2) Press the MENU Key to display the Page Menu Window. Figure 8-8 Invert Flight Plan

Figure 8-9 Invert Flight Plan Conﬁrmation

Figure 8-6 Delete Flight Plan 8.7 CREATE A NEW FLIGHT PLAN

3) Turn the large FMS Knob to highlight ‘Delete Create a New Flight Plan Using the MFD Flight Plan’ and press the ENT Key. With ‘OK’ 1) Press the FPL Key and turn the small FMS Knob highlighted, press the ENT Key to deactivate to display the Flight Plan Catalog Page. Garmin G1000 Cockpit Reference Guide for the DA40 8-3 SECTION 8 – FLIGHT PLANNING

2) Press the NEW Softkey to display a blank flight plan window for the first empty storage NOTE: After the first leg is entered (using the location. PFD only), it is immediately activated.

1) Press the FPL Key, then press the FMS Knob to activate the cursor. 2) Turn the small FMS Knob to enter the first letter of the destination waypoint identifier. Turn the Figure 8-10 Create FPL on MFD large FMS Knob to the right to move the cursor 3) Turn the small FMS Knob to display the to the next character position. Waypoint Information Window. 3) Repeat step 2 to spell out the rest of the 4) Turn the small FMS Knob to enter the first waypoint identifier. character of the identifier of the departure 4) Press the ENT Key and the cursor is now ready waypoint. for entering of the next flight plan waypoint. 5) Turn the large FMS Knob to move the cursor to 5) Repeat steps 2 through 4 to enter the identifier the next character field. Repeat steps 4 and 5 for each additional flight plan waypoint. until the desired identifier has been entered. 6) Once all waypoints have been entered, press the FMS Knob remove the cursor. The new flight plan is now active.

Figure 8-11 Waypoint Info Window 6) Press the ENT Key. Figure 8-12 Creating Flight Plan on the PFD 7) Repeat steps 3 through 5 to enter the identifier for each additional flight plan waypoint. 8.8 LOAD A DEPARTURE 8) When all waypoints have been entered, press See the Procedures section for a discussion on loading the FMS Knob to return to the Flight Plan and activating departure procedures. Catalog Page. The new flight plan is now in the list. 8.9 LOAD AN ARRIVAL Create a New Flight Plan Using the PFD See the Procedures section for a discussion on loading and activating arrival procedures. NOTE: A flight plan cannot be entered using the PFD if another flight plan is active.

8-4 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 8 – FLIGHT PLANNING

8.10 LOAD AN APPROACH 2) Press the FMS Knob to activate the cursor. See the Procedures section for a discussion on loading 3) Turn the large FMS Knob to highlight the and activating approach procedures. desired flight plan and press the ENT Key. 4) Turn the large FMS Knob to place the cursor in 8.11 REMOVE A DEPARTURE, ARRIVAL, the desired locations for entering changes. OR APPROACH FROM A FLIGHT PLAN 5) Turn the FMS Knobs to make the desired changes, then press the ENT Key. 1) With the Active or Stored Flight Plan Page 6) Press the FMS Knob to return to the Flight Plan displayed, press the FMS Knob to activate the Catalog Page. cursor. 2) Turn the large FMS Knob to highlight the title 8.14 DELETE A WAYPOINT FROM THE for the approach, departure or arrival to be FLIGHT PLAN deleted. Titles appear in white directly above the procedure’s waypoints. 1) With either the Active or Stored Flight Plan 3) Press the CLR Key to display a confirmation displayed, press the FMS Knob to activate the window. With ‘OK’ highlighted, press the ENT cursor. Key to remove the selected procedure. 2) Turn the large FMS Knob to select the waypoint to be deleted. 8.12 STORE A NEWLY CREATED FLIGHT 3) Press the CLR Key to display a ‘REMOVE (Wpt PLAN Name)’ confirmation window. 1) After creating a flight plan on either the PFD or MFD, it may be saved by pressing the MENU Key. 2) Turn the large FMS Knob to highlight ‘Store Figure 8-14 Remove Waypoint Confirmation Flight Plan’ and press the ENT Key. 4) With ‘OK’ highlighted, press the ENT Key to 3) With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel the delete store the flight plan. request, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. 5) Once all changes have been made, press the FMS Knob to remove the cursor. Figure 8-13 Store Flight Plan Confirmation 8.13 EDIT A STORED FLIGHT PLAN 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.

Garmin G1000 Cockpit Reference Guide for the DA40 8-5 SECTION 8 – FLIGHT PLANNING

8.15 INVERT AND ACTIVATE A STORED is displayed. With ‘OK’ highlighted, press the FLIGHT PLAN ENT Key to delete the flight plan. To cancel, turn the large FMS Knob to highlight ‘CANCEL’ 1) From the Flight Plan Catalog Page, press the and press the ENT Key. FMS Knob to activate the cursor. 8.18 GRAPHICAL FLIGHT PLAN CREATION 2) Turn the large FMS Knob to highlight the desired flight plan. 1) Press the FPL Key to display the Active Flight 3) Press the INVERT Softkey. ‘Invert and activate Plan Page. stored flight plan?’ will be displayed. 2) Press the Joystick to activate the map pointer. 4) With ‘OK’ highlighted, press the ENT Key. Use the Joystick to move the pointer to the The selected flight plan is now inverted and desired point on the map to be inserted as a activated. The original flight plan remains waypoint in the flight plan. intact in its flight plan catalog storage 3) Press the LD WPT Softkey. The selected location. waypoint will be inserted at the end of the flight plan. The default user waypoint naming 8.16 COPY A FLIGHT PLAN is USR000, USR001, USR002 and so on. 1) From the Flight Plan Catalog press the FMS 4) If the selected waypoint is to be placed Knob to activate the cursor elsewhere in the flight plan, press the FMS 2) Turn the large FMS Knob to highlight the flight Knob to activate the cursor. Waypoints are plan to be copied. inserted ABOVE the cursor. 3) Press the COPY Softkey. 5) After placing the cursor at the desired point in the list of waypoints, press the LD WPT 4) A ‘Copy to flight plan #?’ confirmation window Softkey. is displayed. With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel, turn 6) To change the user waypoint name, follow the the large FMS Knob to highlight ‘CANCEL’ and procedure for modifying a user waypoint. press the ENT Key. 8.19 TRIP PLANNING 8.17 DELETE A FLIGHT PLAN 1) Turn the large FMS Knob to select the ‘AUX’ 1) From the Flight Plan Catalog Page, press the page group. FMS Knob to activate the cursor. 2) Turn the small FMS Knob to select the first 2) Turn the large FMS Knob to highlight the flight rectangular page icon. plan to be deleted. 3) The current page mode is displayed at the 3) Press the DELETE Softkey. top of the page: ‘AUTOMATIC’ or ‘MANUAL’. 4) A ‘Delete flight plan #?’ confirmation window To change the page mode, press the AUTO or MANUAL Softkey.

8-6 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 8 – FLIGHT PLANNING

Starting WPT Ending WPT the small FMS Knob to select the desired flight plan (already stored in memory), by number. Turn the large FMS Knob to highlight the ‘LEG’ field and turn the small FMS Knob to select the desired leg of the flight plan, or select ‘CUM’ to apply trip planning calculations to the entire flight plan. Selecting ‘FPL 00’ will display an active flight plan. If an active flight plan is selected, ‘REM’ will be an available option to display planning data for the remainder of the flight plan.

NOTE: The Page Mode must be set to MANUAL to perform the following steps.

Figure 8-15 Trip Planning Page 7) Turn the large FMS Knob to highlight the departure time (DEP TIME) field. 4) For Direct-to planning, press the WPTS Softkey and verify that the starting waypoint 8) Turn the FMS Knobs to enter the departure time. field indicates ‘P.POS’ (present position). If Press the ENT Key when finished. (Departure necessary, press the MENU Key and select ‘Set time may be entered in local or UTC time, WPT to Present Position’ to display ‘P.POS’. depending upon system settings). Press the ENT Key and the flashing cursor 9) Turn the FMS Knobs to enter the fuel flow. moves to the ending waypoint field. Turn the Press the ENT Key when finished. Note that FMS Knobs to enter the identifier of the ending in automatic page mode, fuel flow is provided waypoint and press the ENT Key to accept the by the system. waypoint. OR, 10) The flashing cursor moves to the fuel on board 5) For point-to-point planning, turn the FMS field. Turn the FMS Knobs to modify the fuel Knobs to enter the identifier of the starting on board. Press the ENT Key when finished. In waypoint. Once the waypoints identifier ‘AUTOMATIC’ mode, fuel onboard is provided is entered, press the ENT Key to accept the by the entry made in ‘GAL REM’ on the EIS waypoint. The flashing cursor moves to the System Page. ending waypoint. Again, turn the FMS Knobs 11) The flashing cursor moves to the calibrated to enter the identifier of the ending waypoint airspeed field. Turn the FMS Knobs to enter a and press the ENT Key to accept the waypoint. calibrated airspeed. Press the ENT Key when OR, finished. 6) For flight plan leg planning, press the FPL Softkey (at the bottom of the display) and turn

Garmin G1000 Cockpit Reference Guide for the DA40 8-7 SECTION 8 – FLIGHT PLANNING

8.20 VERTICAL NAVIGATION (VNAV) PAGE 5) Press the ENT Key. The cursor is now positioned over the ‘Before’ and ‘After’ field. NOTE: An active flight plan or Direct-to must be 6) Turn the small FMS Knob to select whether the entered in order to utilize VNAV. previously set distance is ‘Before’ or ‘After’ the endpoint. NOTE: VNAV is advisory only and cannot be 7) Press the ENT Key. The cursor is now placed coupled to the autopilot. over the VNAV profile endpoint field.

Figure 8-16 Vertical Navigation (VNAV) Page

Create a Vertical Navigation Profile 8) Turn the small FMS Knob to display a list 1) Press the FPL Key. possible VNAV profile endpoints. When using a 2) Turn the small FMS Knob to select the third flight plan, the target reference waypoint itself page icon. can be specified from the waypoints contained 3) Press the FMS Knob to activate the cursor. in the flight plan. By default, the last waypoint in the flight plan is selected. Highlight the 4) With the ‘TARGET POSITION’ distance field desired waypoint. highlighted, turn the FMS Knobs to select the desired distance for Top Of Climb or Bottom Of 9) Press the ENT Key. Descent from the VNAV profile endpoint. The 10) With the ‘TARGET ALTITUDE’ field highlighted, default distance is 4 nm. turn the small and large FMS Knobs to select

8-8 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 8 – FLIGHT PLANNING

the target altitude. If the selected altitude is above the current aircraft altitude, a profiled climb is created. If the selected altitude is below the current aircraft altitude, a profiled descent will be created. 11) Press the ENT Key. The cursor is now placed Figure 8-17 Approaching VNAV Profile Message (PFD) in the ‘TARGET VERTICAL SPEED’ field. The default profile utilizes a 400 foot-per-minute descent rate. 12) To change the vertical speed, turn the FMS Knobs to enter the desired vertical speed. Press the ENT Key when finished. Figure 8-18 Approaching Target Altitude Message (PFD) With the profile set, the vertical speed required (VSR) is displayed. Expect the following to occur when using the To display map data on the Vertical Navigation Map vertical navigation feature: Page, press the MAP Softkey. Press the TOPO, TERRAIN, or LTNG Softkey. Press the same softkey to remove the At one minute prior to reaching the Bottom Of Climb displayed data from the Vertical Navigation Page. or Top Of Descent point (gray arc), the message ‘APPR VPROF - Approaching VNAV Profile’ is displayed as a PFD VNAV Page Menu Options alert. The descent (or climb) angle also locks to prevent The VNAV messages are not enabled until the ‘VNAV changes in speed from altering the profile. If selected, Messages On?’ option is enabled from the VNAV Page the vertical speed required (VSR) readout on the default Menu Options. To display the page menu, press the NAV and map pages shows the desired vertical speed to MENU Key (with the VNAV Page displayed). The VNAV maintain the proper descent (or climb) angle. At 500 feet Page Options Menu also allows the pilot to restore VNAV above (or below, for a climb) the target altitude (white page defaults. arc), an ‘APPR TRG ALT’ - Approaching Target Altitude” message is provided. The VSR readout on the Navigation Map Page is blanked out at this point.

Garmin G1000 Cockpit Reference Guide for the DA40 8-9 SECTION 8 – FLIGHT PLANNING

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8-10 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 9 – PROCEDURES

SECTION 9: PROCEDURES

9.1 ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure

1) With the Navigation Map Page displayed, press Figure 9-2 Select Departure Transition the FPL Key. 2) Press the LD DP Softkey. If a flight plan is active, 8) With ‘LOAD?’ highlighted, press the ENT Key. the departure airport will be displayed as the The departure will be active when the flight default. A list of available departures is also plan is active. displayed. 3) If no flight plan is active, use the FMS Knobs Load and Activate an Arrival Procedure to enter the identifier of the desired airport. 1) With the Navigation Map Page displayed, press Press the ENT Key. the FPL Key. 4) Turn the large FMS Knob to highlight the 2) Press the LD STAR Softkey. If a flight plan is Departure field. Turn the small FMS Knob to active, the destination airport will be displayed display a list of available departures. as the default. A list of available arrivals is also 5) Turn either FMS Knob to select the desired displayed. departure and press the ENT Key. 3) If no flight plan is active, use the FMS Knobs to enter the identifier of the desired airport. Press the ENT Key. 4) Turn the large FMS Knob to highlight the Arrival field. Turn the small FMS Knob to display a list of available arrivals. 5) Turn either FMS Knob to select the desired arrival and press the ENT Key. Figure 9-1 Select Departure 6) A list of runways may be displayed for the departure. Turn either FMS Knob to select the desired runway and press the ENT Key. 7) A list of available transitions is displayed for the departure. Turn either FMS Knob to highlight the desired transition waypoint and press the Figure 9-3 Select Arrival ENT Key.

Garmin G1000 Cockpit Reference Guide for the DA40 9-1 SECTION 9 – PROCEDURES

6) A second window is displayed listing available will not have this designation, meaning the GPS receiver transitions for the arrival. Turn either FMS Knob can be used for supplemental navigation guidance only. to highlight the desired transition waypoint and If the GPS receiver cannot be used for primary guidance, press the ENT Key. the appropriate navigation receiver must be used for the selected approach (e.g., VOR or ILS). The final course segment of ILS approaches, for example, must be flown by tuning the Nav receiver to the proper frequency and selecting that Nav receiver on the CDI. Load and/or Activate an Approach Procedure 1) With the Navigation Map Page displayed, press Figure 9-4 Select Arrival Transition the FPL Key. 7) A third window is displayed listing the available 2) Press the LD APR Softkey. If a flight plan is runways. Turn either FMS Knob to select the active, the destination airport will be displayed desired runway and press the ENT Key. as the default. A list of available approaches is also displayed. 3) If no flight plan is active, use the FMS Knobs to enter the identifier of the desired airport. Press the ENT Key. 4) Turn the large FMS Knob to highlight the Approach field. Turn the small FMS Knob to display a list of available approaches.

Figure 9-5 Select Arrival Runway 8) With ‘LOAD?’ highlighted, press the ENT Key. If a flight plan is active, the selected arrival procedure is inserted after the destination airport and becomes part of the active flight plan. If no flight plan is active when the arrival is loaded, the arrival procedure will become the active flight plan. 9.2 APPROACHES Not all approaches in the database are approved for GPS Figure 9-6 Selecting an Approach Procedure use. When selecting an approach, a “GPS” designation to 5) Turn the FMS Knobs to highlight the desired the right of the procedure name indicates the procedure approach. Press the ENT Key. can be flown using the GPS receiver. Some procedures

9-2 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 9 – PROCEDURES

6) The cursor will move to the TRANSITIONS field. Turn the large FMS Knob to highlight the desired transition waypoint and press the ENT Key. (The “Vectors” option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course.)

Figure 9-7 Selecting an Approach Transition

7) Turn the large FMS Knob to highlight ‘Activate?’ and press the ENT Key to activate the approach. Selecting ‘Load?’ will add the procedure to the ﬂight plan without immediately using it for navigation guidance. Activate An Approach in the Active Flight Plan 1) With the Navigation Map Page displayed, press the PROC Key. 2) Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’. 3) Press the ENT Key. The approach procedure is now active.

Garmin G1000 Cockpit Reference Guide for the DA40 9-3 SECTION 9 – PROCEDURES

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9-4 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 10 – HAZARD AVOIDANCE

SECTION 10: HAZARD AVOIDANCE 10.2 XM WEATHER (OPTIONAL) 10.1 CUSTOMIZING THE HAZARD WARNING: XM Weather is not intended to be used for hazardous weather penetration. DISPLAYS ON THE NAVIGATION MAP Weather information provided by XM Radio 1) With the Navigation Map Page displayed, press Service is approved only for weather avoidance, not penetration. the MENU Key to display the Navigation Map Page Menu. The cursor flashes on the ‘Map 1) Press the MAP Softkey. Setup’ option. 2) Press the NEXRAD or XM LTNG Softkey to 2) Press the ENT Key. The Map Setup Menu is display the desired weather. Press the displayed. Turn the small FMS Knob to select applicable softkey again to remove weather the ‘Weather’ or ‘Traffic’ group to customize data from the Navigation Map Page. the display of weather features. Select ‘Traffic’ to customize the display of traffic. 3) Press the small FMS Knob to return to the Navigation Map Page.

Figure 10-1 Page Menu

Figure 10-4 Navigation Map Page Displaying NEXRAD Weather

Displaying METAR and TAF information on the Airport Information Page Figure 10-2 Map Setup Menu To display METAR and TAF text on the Airport Information Page: 1) Turn the large FMS Knob to select the WPT Page Group. 2) Turn the small FMS Knob to select the Airport Figure 10-3 Map Setup Group List Information Page.

Garmin G1000 Cockpit Reference Guide for the DA40 10-1 SECTION 10 – HAZARD AVOIDANCE

3) Press the WX Softkey to display METAR and TAF text (METAR and TAF information is updated every 12 minutes).

METAR Text

TAF Text Figure 10-6 Weather Data Link Page NEXRAD – Press the NEXRAD Softkey to show NEXRAD weather and radar coverage information. WX Softkey Areas where radar coverage is not available will be shown in grayish-purple. The display is updated Figure 10-5 METAR and TAF Text Displayed on the every five minutes. Airport (Weather) Information Page NEXRAD Limitations Displaying Weather on the Weather Data Link Certain limitations exist regarding the NEXRAD radar Page displays. Some, but not all, are listed here: To select the Weather Data Link Page: • NEXRAD base reflectivity does not provide 1) Turn the large FMS Knob to select the Map sufficient information to determine cloud layers or Page Group. precipitation characteristics (hail vs. rain, etc). 2) Turn the small FMS Knob to select the fourth • An individual NEXRAD site cannot depict high rectangular page icon. altitude storms at close ranges, and has no information about storms directly over the site. 3) Press the available softkeys to select the desired • The resolution of displayed NEXRAD data is 2 XM weather product. kilometers. Therefore, when zoomed in on the 4) Press the LEGEND Softkey to view the legends display, each square block is 2 kilometers on each for the selected products. If necessary, turn the side. The intensity level reflected by the square FMS Knobs to scroll through the list. Press the will be the highest level sampled within the square small FMS Knob or the ENT Softkey to return area. to the map.

10-2 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 10 – HAZARD AVOIDANCE

ECHO TOP – Press the ECHO TOP Softkey to show SFC – Pressing the SFC Softkey for Surface Analysis the location, elevation, and direction the highest shows current or forecast conditions. Forecasts radar echo. This may not indicate the top of a are available for intervals of Current, 12, 24, 36, storm or clouds, only the highest radar return and 48 hours. Press the softkey corresponding echo. ECHO TOPS cannot be displayed along to the desired forecast. The closest city forecast with NEXRAD and CLOUD TOPS. When ECHO information is displayed in the legend. The TOPS is activated, NEXRAD and CLOUD TOPS are display is updated every 12 minutes. removed. Refer to the Legend for a description of FRZ LVL – Press the FRZ LVL Softkey to display the ECHO TOPS coding. The display is updated contour lines for freezing levels. The display is every 7.5 minutes. updated every 12 minutes. CLD TOP – Press the CLD TOP Softkey to show the WIND – Press the WIND Softkey to show wind cloud top altitude determined from satellite imagery. speed and direction at a selected altitude from The display is updated every 15 minutes. the ground up to 42,000 feet in 3,000 foot increments. After pressing the WIND Softkey, LTNG – Pressing the LTNG Softkey shows the location press the softkey corresponding to the desired of cloud-to-ground lightning strikes. The display is winds aloft altitude. The display is updated every updated every five minutes. 12 minutes. NOTE: Strikes depicted represent cloud to ground COUNTY – Pressing the COUNTY Softkey provides strikes within a 2 kilometer radius of the actual specific public awareness and protection weather strike location. Therefore, the exact location of warnings for Tornado, Severe Thunderstorm, the strike is not displayed. and Flood conditions provided by the National Weather Service (NWS). The display is updated CELL MOV – Pressing the CELL MOV Softkey shows every 5 minutes. storm cell movement by displaying an arrow. CYCLONE – Pressing the CYCLONE Softkey shows pointing in the direction of predicted movement. the current location of cyclones (hurricanes and The display is updated every 12 minutes. tropical storms) and their projected track at SIG/AIR – Pressing the SIG/AIR Softkey shows various time intervals. The display is updated SIGMET and AIRMET information. The display is every 12 minutes. updated every 12 minutes. Map Panning Information – Weather Data Link METAR – Press the METAR Softkey to graphically Page display METARs. METARS are shown as colored flags at airports providing METAR reports. The 1) Push in the Joystick to display the panning display is updated every 12 minutes. arrow. MORE WX – Press the MORE WX Softkey to display 2) Move the Joystick to place the panning arrow the following group of softkeys for additional on AIRMETs, TFRs, METARs, or SIGMETs. Press weather control: the ENT Key to display pertinent information for the selected product.

Garmin G1000 Cockpit Reference Guide for the DA40 10-3 SECTION 10 – HAZARD AVOIDANCE

Note that pressing the ENT Key when panning The XM Information Page in the AUX Page Group will over an AIRMET or a SIGMET displays an display the weather products available for the current information box that displays the text of the subscription. A green box by the weather product means report. Panning over an airport with METAR that it is available. information does not display more information but allows the user to press the ENT Key and NOTE: The DONE Softkey on the AUX - XM

select that Airport’s Information Page to display INFORMATION Page is used to save the GDL the text of the report. Pressing the ENT Key 69(A) activation data when the XM services are initially set up. It is not used during normal when panning over a TFR displays TFR speciﬁc operation of the GDL 69(A), and it should have information. no adverse effects if inadvertently selected during Weather Products and Symbols ﬂight. Refer to the GDL 69/69A XM Satellite Radio Activation Instructions (190-00355-04, Rev Figure 10-7 depicts the symbol for each weather E or later) for further information. product (read from left to right). When a weather product is active, the product symbol is displayed in the lower right of the screen. Weather Product Age • NEXRAD The age for each of the enabled products is displayed • Cloud Top/Echo Top on the right side of the display. Times are based on Zulu • XM Lightning time when the data was assembled on the ground, not the • Cell Movement time the data was received by the FIS sensor. When the age • SIGMETs/AIRMETs of a weather product has exceeded half of the expiration • METARs time, the product time will change from light blue to amber • City Forecast in color. • Surface Analysis • Freezing Levels • Winds Aloft • County Warnings • Cyclone Warnings

Echo Top (Cloud Top and Echo Top Mutually Exclusive)

Figure 10-7 Weather Product Symbols

10-4 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 10 – HAZARD AVOIDANCE

10.3 TRAFFIC INFORMATION SERVICE (TIS) Weather Product Expires After (minutes) NOTE: Traffic Information Service (TIS) is only SIGMETs/AIRMETs 60 available when the aircraft is within the service City Forecasts 60 volume of a TIS capable terminal radar site. County Warnings 60 Displaying Traffic on the Traffic Map Page Cyclone Warnings 60 Echo Tops 30 1) Turn the large FMS Knob to select the Map Freezing Levels 60 Page Group. METARs 90 2) Turn the small FMS Knob to select the second Lightning 30 rectangular page icon. NEXRAD 30 3) Press the OPERATE Softkey to begin displaying traffic. ‘TIS OPERATIING’ is displayed in the Radar Coverage 30 Traffic Mode field. Cell Movement 30 4) Press the STANDBY Softkey to place the system Surface Analysis 60 in the Standby mode. ‘TIS STANDBY’ will be TFRs 60 displayed in the Traffic Mode field. Winds Aloft 90 5) Rotate the Joystick clockwise to display a larger TAFs 60 area or rotate counter-clockwise to display a Clouds Tops 60 smaller area. If data is not received for a period longer than 6 seconds, the age of the present data will be displayed in the lower left of of the screen along with the annuciation that the system has entered Coast mode. The system will maintain the traffic display (up to 60 seconds) until the next data reception. If no data is received after 60 seconds, traffic will be removed from the display.

Garmin G1000 Cockpit Reference Guide for the DA40 10-5 SECTION 10 – HAZARD AVOIDANCE

Traffic Advisory, aircraft is 400’ above & Traffic out of Traffic Mode descending, moving in the direction of the line range 10.4 TERRAIN AND OBSTACLE PROXIMITY

NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.

Displaying Terrain and Obstacles on the Terrain Proximity Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the last rectangular page icon. 3) If desired, press the VIEW Softkey to access the ARC and 360 Softkeys. When the ARC Softkey Last data update Proximity Traffic at same Traffic 1600’ above & is older than 6 altitude, level flight & moving climbing, moving in the is pressed, a radar-like 120° view is displayed. sec. resulting in in the direction of the line direction of the line Press the 360 Softkey to return to the 360° Coast mode Figure 10-8 Traffic Map Page default display. 4) Rotate the Joystick clockwise to display a larger Displaying Traffic on the Navigation Map area or rotate counter-clockwise to display a 1) Ensure TIS is operating. With the Navigation smaller area. Map displayed, press the MAP Softkey. 2) Press the TRAFFIC Softkey. Traffic will now be displayed on the map. TIS Audio Alert When a Traffic Advisory (TA) is displayed, an audio alert “Traffic” is given. “Traffic Not Available” will be heard whenever TIS service becomes unavailable.

Figure 10-9 Terrain Proximity Page

10-6 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 10 – HAZARD AVOIDANCE

Color Indication Displaying Terrain and Obstacles on the WARNING: Terrain/Obstacle at or within Navigation Map RED 100’ below or above aircraft altitude. 1) With the Navigation Map displayed, press the CAUTION: Terrain/Obstacle between 100’ MAP Softkey. YELLOW and 1000’ below current aircraft altitude. 2) Press the TERRAIN Softkey. Terrain and obstacle proximity will now be displayed on the map. Aircraft Altitude 100' Threshold Maximum 1000' elevation of topography presently displayed on-screen Minimum elevation of topography presently displayed on-screen

Aircraft altitude

Range of topography eleva- Ground elevation tion presently dis- at present aircraft played on-screen position

Figure 10-10 Topography Scale

Unlighted Obstacle Lighted Obstacle Unlighted Obstacle Lighted Obstacle (Height is less than (Height is less than (Height is greater than (Height is greater than 1000’ AGL) 1000’ AGL) 1000’ AGL) 1000’ AGL)

Figure 10-11 Obstacle Symbols

Garmin G1000 Cockpit Reference Guide for the DA40 10-7 SECTION 10 – HAZARD AVOIDANCE

Blank Page

10-8 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 11 – ABNORMAL OPERATION

SECTION 11: ABNORMAL Reversionary display mode can also be manually activated by the pilot if the system fails to detect a display OPERATION problem. The reversionary mode is activated manually by pressing the red DISPLAY BACKUP button on the bottom of the audio panel (GMA 1347). Pressing the red 11.1 REVERSIONARY MODE DISPLAY BACKUP button again deactivates reversionary Should a system detected failure occur in either display, mode. the G1000 automatically enters reversionary mode. In reversionary mode, critical ﬂight instrumentation is NOTE: The Diamond DA40 Airplane Flight Manual combined with engine instrumentation on the remaining and Flight Manual Supplement always takes precedence over the information found in this display. Minimal navigation capability is available on the section. reversionary mode display.

Normal PFD Display Normal MFD Display

MFD in Reversionary Mode

Figure 11-1 G1000 Reversionary Mode: Failed PFD

Garmin G1000 Cockpit Reference Guide for the DA40 11-1 SECTION 11 – ABNORMAL OPERATION

11.2 ABNORMAL COM OPERATION 11.5 HAZARD DISPLAYS WITH LOSS OF When a COM tuning failure is detected by the system, GPS POSITION the emergency frequency (121.500 MHz) is automatically If GPS position is lost, or becomes invalid, selected loaded into the active frequency ﬁeld of the COM radio hazards being displayed on the Navigation Map Page for which the tuning failure was detected. In the event of will be removed until GPS position is again established. a dual display failure, the emergency frequency (121.500 The icons in the lower right of the screen, indicating the MHz) automatically becomes the active frequency to the selected functions for display, will show an ‘X’, as shown pilot through the pilot headset. in Figure 11-3. 11.3 UNUSUAL ATTITUDES The PFD will ‘declutter’ when the aircraft enters an unusual attitude. Only the basic primary functions will be displayed in these situations. Figure 11-3 Loss of Hazard Functions with Loss of GPS Position Red extreme pitch warning chevrons pointing toward the horizon are displayed starting at 50 degrees above and 30 degrees below the horizon line.

Figure 11-2 Extreme Pitch Indication

11.4 STORMSCOPE OPERATION WITH LOSS OF HEADING INPUT If heading is lost, strikes and/or cells must be cleared manually after the execution of each turn. This is to ensure that the strike and/or cell positions are depicted accurately in relation to the nose of the aircraft.

11-2 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 12 – ANNUNCIATIONS & ALERTS

SECTION 12: ANNUNCIATIONS & from annunciations that are not yet acknowledged. Acknowledged annunciations are always above ALERTS the line. Annunciations are displayed in order of priority from top to bottom. The highest NOTE: The Airplane Flight Manual Supplement priority annunciation is displayed at the top of the

supersedes information found in this Annunciation Window. document. • Alerts Window: The Alerts Window displays alert text messages. Up to 64 prioritized alerts can be displayed in the Alerts Window. Pressing the ALERTS Softkey displays the Alerts Window. Pressing the ALERTS Softkey again removes the Alerts Window from the display. When the Alerts System Window is displayed, the pilot may use the large Annunciation Red ‘X’ FMS Knob to scroll through the alert list. Higher priority alerts are displayed at the top of the window. Lower priority alerts are displayed at the bottom of Annunciation the window. Active alerts are displayed in white Window text. Alerts that have become inactive will change to gray text. The ALERTS Softkey will flash if the state of a displayed alert changes or a new alert is displayed. The inactive alerts can be removed from Alerts Window the Alerts Window by pressing the flashing ALERTS Softkey. • ALERTS Softkey Annunciation: When the ALERTS Softkey Alerting System issues an alert, the ALERTS Softkey Annunciation is used as a flashing annunciation to accompany Figure 12-1 G1000 Alerting System an alert. During the alert, the ALERTS Softkey The G1000 Alerting System conveys alerts to the pilot assumes a new label consistent with alert level using a combination of the following items: (WARNING, CAUTION, or ADVISORY). Pressing the softkey annunciation acknowledges that the • Annunciation Window: The Annunciation pilot is aware of the alert. The softkey then returns Window displays abbreviated annunciation text. to the previous ALERTS label. The pilot can then The Annunciation Window is located to the right press the ALERTS Softkey again to view alert text of the Altitude and Vertical Speed Boxes on the PFD messages. display (or the MFD if system is in reversionary mode). Up to 12 DA40 annunciations can be • System Annunciations: Typically, a large red ‘X’ displayed simultaneously. A white horizontal line appears in a window when a related LRU fails or separates annunciations that are acknowledged detects invalid data.

Garmin G1000 Cockpit Reference Guide for the DA40 12-1 SECTION 12 – ANNUNCIATIONS & ALERTS

• Audio Alerting System: The G1000 system issues audio alert tones when specific system conditions are met. See the Alert Levels Definitions section for Figure 12-2 WARNING Softkey more information. Annunciation 12.1 ALERT LEVEL DEFINITIONS The G1000 Alerting System, as installed in Diamond DA40 aircraft, uses three alert levels. • WARNING: This level of alert requires immediate pilot attention. A warning alert is accompanied Figure 12-3 CAUTION Softkey by an annunciation in the Annunciation Window. Annunciation Warning text appearing in the Annunciation Window is RED. A warning alert is also accompanied by a flashing WARNING Softkey annunciation, as shown in Figure 12-2. Pressing the WARNING Softkey acknowledges the presence of the warning alert and stops the aural tone, if applicable.

• CAUTION: This level of alert indicates the Figure 12-4 ADVISORY Softkey existence of abnormal conditions on the aircraft Annunciation that may require pilot intervention. A caution alert is accompanied by an annunciation in the Annunciation Window. Caution text appearing in the Annunciation Window is YELLOW. A caution alert is also accompanied by a ﬂashing CAUTION Softkey annunciation, as shown in Figure 12-3. Pressing the CAUTION Softkey acknowledges the presence of the caution alert. • MESSAGE ADVISORY: This level of alert provides general information to the pilot. A message advisory alert does not issue annunciations in the Annunciation Window. Instead, message advisory alerts only issue a ﬂashing ADVISORY Softkey annunciation, as shown in Figure 12-4. Pressing the ADVISORY Softkey acknowledges the presence of the message advisory alert and displays the alert text message in the Alerts Window.

12-2 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 12 – ANNUNCIATIONS & ALERTS

12.2 AIRCRAFT ALERTS The following alerts are conﬁgured speciﬁcally for the Diamond DA40 aircraft. See the Flight Manual Supplement for information regarding pilot responses.

WARNING Alerts Annunciation Window Text Alerts Window Message Audio Alert OIL PRES LO Oil pressure is below 25 psi. FUEL PRES LO Fuel pressure is below 14 psi. (1.0 psi on DA40F) FUEL PRES HI Fuel pressure is greater than 35 psi. (8 psi on DA40F) ALTERNATOR Alternator failed. Battery is only electrical source. Continuous Aural Tone STARTER ENGD Starter is engaged. DOOR OPEN Canopy and/or rear door is not closed and locked. TRIM FAIL Autopilot automatic trim is inoperative.

CAUTION Alerts

Annunciation Window Text Alerts Window Message Audio Alert L FUEL LOW Left fuel quantity is less than 3 gallons. R FUEL LOW Right fuel quantity is less than 3 gallons. LOW VOLTS On-board voltage is below 24 V. Single Aural Tone PITOT FAIL Pitot heat is inoperative. PITOT OFF Pitot heat is off.

Message Advisory Alerts Alerts Window Message Audio Alert PFD FAN FAIL – The cooling fan for the PFD is inoperative. MFD FAN FAIL – The cooling fan for the MFD is inoperative. None GIA FAN FAIL – The cooling fan for the GIAs is inoperative.

Garmin G1000 Cockpit Reference Guide for the DA40 12-3 SECTION 12 – ANNUNCIATIONS & ALERTS

12.3 AFCS ALERTS System Status Annunciation

System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD.

Figure 12-5 AFCS System Status Annunciation Condition Annunciation Description Pitch Failure Pitch axis control failure. AP is inoperative.

Roll Failure Roll axis control failure. AP is inoperative.

AP TRIM Switch Stuck, If annunciated when AP is engaged, a failure has occurred in the pitch trim system. If or Pitch Trim Axis annunciated when AP is not engaged, a failed or stuck switch is causing the annunciation. Control Failure System Failure AP and manual electric trim (AP TRIM) are unavailable. FD may still be available.

Elevator Mistrim Up A condition has developed causing the pitch servo to provide a sustained force in the nose up direction. Elevator Mistrim A condition has developed causing the pitch servo to provide a sustained force in the nose Down down direction. Aileron Mistrim Left A condition has developed causing the roll servo to provide a sustained left force.

Aileron Mistrim Right A condition has developed causing the roll servo to provide a sustained right force.

Preflight Test Performing preflight system test. Upon completion of the test, the aural alert will be heard. Preflight system test has failed.

12-4 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 12 – ANNUNCIATIONS & ALERTS

12.4 G1000 SYSTEM ANNUNCIATIONS NOTE: Upon power-up of the G1000 system, When an LRU or an LRU function fails, a large red certain windows remain invalid as G1000 ‘X’ is typically displayed on windows associated with the equipment begins to initialize. All windows failed data. The following section describes various system should be operational within one minute of annunciations. Refer to the Airplane Flight Manual for power-up. Should any window continue to additional information regarding pilot responses to these remain ﬂagged, the G1000 system should be annunciations. serviced by a Garmin-authorized repair facility.

System Annunciation Comment

Attitude and Heading Reference System is aligning.

Display system is not receiving attitude information from the AHRS.

Display system is not receiving airspeed input from air data computer.

Display is not receiving altitude input from the air data computer.

Garmin G1000 Cockpit Reference Guide for the DA40 12-5 SECTION 12 – ANNUNCIATIONS & ALERTS

System Annunciation Comment

Display is not receiving vertical speed input from the air data computer.

Display is not receiving valid heading input from AHRS.

GPS information is either not present or is invalid for navigation use. Note that AHRS utilizes GPS inputs during normal operation. AHRS operation may be degraded if GPS signals are not present (see AFMS).

Display is not receiving valid transponder information. A red ‘X’ through any other display field, such as engine instrumentation Other Various Red X Indications fields, indicates that the field is not receiving valid data.

12-6 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 12 – ANNUNCIATIONS & ALERTS

A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 12-6 illustrates all possible ﬂags and the responsible LRUs.

GIA 63 Integrated GIA 63 Integrated Avionics Units Avionics Units

GDC 74A Air Data Computer

GRS 77 AHRS GEA 71 Engine OR Airframe Unit GMU 44 OR Magnetometer GIA 63 Integrated Avionics Unit

GIA 63 Integrated Avionics Units

GDC 74A Air Data GTX 33 Transponder Computer OR GIA 63 Integrated Figure 12-6 G1000 System Failure Annunciations Avionics Units

12.5 G1000 SYSTEM MESSAGE NOTE: This section provides information regarding G1000 message advisories that may ADVISORIES be displayed by the system. Knowledge of the This section describes various G1000 system message aircraft, systems, ﬂight conditions, and other advisories. Certain messages are issued due to an LRU existing operational priorities must be considered or an LRU function failure. Such messages are normally when responding to a message. Always use sound pilot judgment. The Aircraft Flight Manual accompanied by a corresponding red ‘X’ annunciation takes precedence over any conﬂicting guidance as shown previously in the G1000 System Annunciation found in this section. section.

Garmin G1000 Cockpit Reference Guide for the DA40 12-7 SECTION 12 – ANNUNCIATIONS & ALERTS

MFD & PFD Message Advisories Message Comments DATA LOST – Pilot stored data was The pilot profile data was lost. System reverts to default pilot profile and settings. lost. Recheck settings. The pilot may reconfigure the MFD & PFD with preferred settings, if desired. XTALK ERROR – A flight display The MFD and PFD are not communicating with each other. The G1000 system should crosstalk error has occurred. be serviced. PFD1 SERVICE – PFD1 needs service. Return unit for repair. The PFD and/or MFD self-test has detected a problem. The G1000 system should be MFD1 SERVICE – MFD1 needs serviced. service. Return unit for repair. PFD1 CONFIG – PFD1 configuration error. Config service req’d. The PFD and/or MFD configuration settings do not match backup configuration MFD1 CONFIG – MFD1 configuration memory. The G1000 system should be serviced. error. Config service req’d. SW MISMATCH – GDU software The MFD and PFD have different software versions installed. The G1000 system mismatch. Xtalk is off. should be serviced. MANIFEST – PFD1 software mismatch. Communication halted. The PFD and/or MFD has incorrect software installed. The G1000 system should be MANIFEST – MFD1 software serviced. mismatch. Communication halted. PFD1 COOLING – PFD1 has poor cooling. Reducing power usage. The PFD and/or MFD is overheating and is reducing power consumption by dimming MFD1 COOLING – MFD1 has poor the display. If problem persists, the G1000 system should be serviced. cooling. Reducing power usage. PFD1 “KEY” KEYSTK – Key is stuck. A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by press- MFD1 “KEY” KEYSTK – Key is stuck. ing it several times. The G1000 system should be serviced if the problem persists. CNFG MODULE – PFD1 configuration The PFD configuration module backup memory has failed. The G1000 system should module is inoperative. be serviced. PFD1 VOLTAGE – PFD1 has low volt- The PFD1 voltage is low. The G1000 system should be serviced. age. Reducing power usage. MFD1 VOLTAGE – MFD1 has low volt- The MFD1 voltage is low. The G1000 system should be serviced. age. Reducing power usage.

12-8 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 12 – ANNUNCIATIONS & ALERTS

Database Message Advisories Alerts Window Message Comments MFD1 DB ERR – MFD1 aviation database error exists. The MFD and/or PFD detected a failure in the aviation database. Attempt to reload PFD1 DB ERR – PFD1 aviation the aviation database. If problem persists, the G1000 system should be serviced. database error exists. MFD1 DB ERR – MFD1 basemap database error exists. The MFD and/or PFD detected a failure in the basemap database. PFD1 DB ERR – PFD1 basemap database error exists. MFD1 DB ERR – MFD1 terrain database error exists. The MFD and/or PFD detected a failure in the terrain database. Ensure that the terrain card is properly inserted in display. Replace terrain card. If problem persists, The PFD1 DB ERR – PFD1 terrain database G1000 system should be serviced. error exists. MFD1 DB ERR – MFD1 obstacle database error exists. The MFD and/or PFD detected a failure in the obstacle database. Ensure that the data card is properly inserted. Replace data card. If problem persists, The G1000 PFD1 DB ERR – PFD1 obstacle system should be serviced. database error exists. MFD1 DB ERR – MFD1 airport terrain database error exists. The MFD and/or PFD detected a failure in the airport terrain database. Ensure that the data card is properly inserted. Replace data card. If problem persists, The G1000 PFD1 DB ERR – PFD1 airport terrain system should be serviced. database error exists. DB MISMATCH – Aviation database The PFD and MFD have different aviation database versions installed. Crossfill is off. version mismatch. Xtalk is off. Install correct aviation database version in both displays. DB MISMATCH – Aviation database The PFD and MFD have different aviation database types installed (Americas, Euro- type mismatch. Xtalk is off. pean, etc.). Crossfill is off. Install correct aviation database type in both displays. DB MISMATCH – Basemap database The PFD and MFD have different basemap database versions installed. Crossfill is version mismatch. Xtalk is off. off. Install correct basemap database version in both displays. DB MISMATCH – Terrain database The PFD and MFD have different terrain database versions installed. Crossfill is off. version mismatch. Xtalk is off. Install correct terrain database version in both displays. DB MISMATCH – Terrain database The PFD and MFD have different terrain database types installed. Crossfill is off. type mismatch. Xtalk is off. Install correct terrain database type in both displays. DB MISMATCH – Obstacle database The PFD and MFD have different obstacle database versions installed. Crossfill is off. version mismatch. Xtalk is off Install correct obstacle database version in both displays.

Garmin G1000 Cockpit Reference Guide for the DA40 12-9 SECTION 12 – ANNUNCIATIONS & ALERTS

Database Message Advisories (Cont.) Alerts Window Message Comments DB MISMATCH – Airport Terrain The PFD and MFD have different airport terrrain databases installed. Crossfill is off. database mismatch. Xtalk is off Install correct airport terrain database in both displays. GMA 1347 Message Advisories Alerts Window Message Comments GMA1 FAIL – GMA1 is inoperative. The audio panel self-test has detected a failure. The audio panel is unavailable. The G1000 system should be serviced. GMA1 CONFIG – GMA1 configuration The audio panel configuration settings do not match backup configuration memory. error. Config service req’d. The G1000 system should be serviced. MANIFEST – GMA1 software The audio panel has incorrect software installed. The G1000 system should be mismatch. Communication halted. serviced. GMA1 SERVICE – GMA1 needs The audio panel self-test has detected a problem in the unit. Certain audio functions service. Return unit for repair. may still be available, and the audio panel may still be usable. The G1000 system should be serviced when possible. BACKUP PATH – Audio panel 1 using The #1 audio panel is using a backup communication path. The G1000 system backup data path. should be serviced when possible. GIA 63 Message Advisories Alerts Window Message Comments GIA1 CONFIG – GIA1 configuration error. Config service req’d. The GIA1 and/or GIA2 configuration settings do not match backup configuration GIA2 CONFIG – GIA2 configuration memory. The G1000 system should be serviced. error. Config service req’d. GIA1 COOLING – GIA1 temperature too low. The GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to GIA2 COOLING – GIA2 temperature warm up to operating temperature. too low. GIA1 COOLING – GIA1 over temperature. The GIA1 and/or GIA2 temperature is too high. If problem persists, the G1000 GIA2 COOLING – GIA2 over system should be serviced. temperature.

12-10 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 12 – ANNUNCIATIONS & ALERTS

GIA 63 Message Advisories (Cont.) Alerts Window Message Comments GIA1 SERVICE – GIA1 needs service. Return the unit for repair. The GIA1 and/or GIA2 self-test has detected a problem in the unit. The G1000 GIA2 SERVICE – GIA2 needs service. system should be serviced. Return the unit for repair. HW MISMATCH – GIA hardware There is a hardware mismatch between GIA1 and GIA2. The G1000 system should mismatch. Communication halted. be serviced. MANIFEST – GIA1 software mismatch. Communication halted. The GIA1 and/or GIA 2 has incorrect software installed. The G1000 system should MANIFEST – GIA2 software mismatch. be serviced. Communication halted. COM1 TEMP – COM1 over temp. Reducing transmitter power. The system has detected an over temperature condition in COM1 and/or COM2. The transmitter will operate at reduced power. If the problem persists, the G1000 system COM2 TEMP – COM2 over temp. should be serviced. Reducing transmitter power. COM1 SERVICE – COM1 needs service. Return unit for repair. The system has detected a failure in COM1 and/or COM2. COM1 and/or COM2 may COM2 SERVICE – COM2 needs still be usable. The G1000 system should be serviced when possible. service. Return unit for repair. COM1 PTT – COM1 push-to-talk key is stuck. The COM1 and/or COM2 external push-to-talk switch is stuck in the enable (or “pressed”) position. Press the PTT switch again to cycle its operation. COM2 PTT – COM2 push-to-talk key If the problem persists, the G1000 system should be serviced. is stuck. COM1 RMT XFR – COM1 remote transfer key is stuck. The COM1 and/or COM2 transfer switch is stuck in the enabled (or “pressed”) position. Press the transfer switch again to cycle its operation. If the problem persists, COM2 RMT XFR – COM2 remote the G1000 system should be serviced. transfer key is stuck. RAIM UNAVAIL – RAIM is not GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity available from FAF to MAP waypoints. Monitoring (RAIM) from the FAF to the MAP waypoints. RAIM UNAVAIL – RAIM is not GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity available. Monitoring (RAIM) for the current phase of flight. POSN ERROR – RAIM has determined When a RAIM position error is detected, GPS is flagged and the system no longer GPS position is in error. provides GPS-based guidance.

Garmin G1000 Cockpit Reference Guide for the DA40 12-11 SECTION 12 – ANNUNCIATIONS & ALERTS

GIA 63 Message Advisories (Cont.) Alerts Window Message Comments DGRD GPS ACC – GPS position GPS position accuracy has been degraded and RAIM is not available. accuracy degraded & RAIM unavailable. GPS1 FAIL – GPS1 is inoperative. A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver is GPS2 FAIL – GPS2 is inoperative. unavailable. The G1000 system should be serviced. GPS1 SERVICE – GPS1 needs service. Return unit for repair. A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still GPS2 SERVICE – GPS2 needs service. be available. The G1000 system should be serviced. Return unit for repair. NAV1 SERVICE – NAV1 needs service. Return unit for repair. A failure has been detected in the NAV1 and/or NAV2 receiver. The receiver may still NAV2 SERVICE – NAV2 needs service. be available. The G1000 system should be serviced. Return unit for repair. NAV1 RMT XFR – NAV1 remote transfer key is stuck. The remote NAV1 and/or NAV2 transfer switch is stuck in the enabled (or “pressed”) state. Press the transfer switch again to cycle its operation. If the problem persists, NAV2 RMT XFR – NAV2 remote the G1000 system should be serviced. transfer key is stuck. G/S1 FAIL – G/S1 is inoperative. A failure has been detected in glideslope receiver 1 and/or receiver 2. The G1000 G/S2 FAIL – G/S2 is inoperative. system should be serviced. G/S1 SERVICE – G/S1 needs service. Return unit for repair. A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver G/S2 SERVICE – G/S2 needs service. may still be available. The G1000 system should be serviced when possible. Return unit for repair.

GEA 71 Message Advisories Alerts Window Message Comments GEA1 CONFIG – GEA1 configuration The GEA 71 configuration settings do not match those of backup configuration error. Config service req’d. memory. The G1000 system should be serviced. MANIFEST – GEA1 software The GEA 71 has incorrect software installed. The G1000 system should be serviced. mismatch. Communication halted. BACKUP PATH – EIS using backup The GEA 71 is using a backup communication path. The G1000 system should be data path. serviced when possible.

12-12 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 12 – ANNUNCIATIONS & ALERTS

GTX 33 Message Advisories Alerts Window Message Comments XPDR1 CONFIG – XPDR1 config error. The transponder configuration settings do not match those of backup configuration Config service req’d. memory. The G1000 system should be serviced. MANIFEST – GTX1 software mismatch. The transponder has incorrect software installed. The G1000 system should be Communication halted. serviced. BACKUP PATH – XPDR1 using backup The #1 transponder is using a backup communications path. The G1000 system data path. should be serviced when possible.

GRS 77 Message Advisories Alerts Window Message Comments AHRS1 TAS – AHRS1 not receiving The #1 AHRS is not receiving true airspeed from the air data computer. The AHRS airspeed. relies on GPS information to augment the lack of airspeed. The G1000 system should be serviced. AHRS1 GPS – AHRS1 using backup The #1 AHRS is using the backup GPS path. Primary GPS path has failed. The G1000 GPS source. system should be serviced when possible. AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving any or any useful GPS information. Check AFMS limita- any GPS information. tions. The G1000 system should be serviced. AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving backup GPS information. The G1000 system should be backup GPS information. serviced. AHRS1 GPS – AHRS1 operating The #1 AHRS is operating exclusively in no-GPS mode. The G1000 system should be exclusively in no-GPS mode. serviced. MANIFEST – GRS1 software mismatch. The AHRS has incorrect software installed. The G1000 system should be serviced. Communication halted. BACKUP PATH – AHRS1 using backup The #1 AHRS is using a backup communications data path. The G1000 system data path. should be serviced when possible. AHRS1 SRVC – AHRS1 Magnetic-field The #1 AHRS earth magnetic field model is out of date. Update magnetic field model model needs update. when practical. GEO LIMITS – AHRS1 too far North/ The aircraft is outside geographical limits for approved AHRS operation. Heading is South, no magnetic compass. flagged as invalid.

Garmin G1000 Cockpit Reference Guide for the DA40 12-13 SECTION 12 – ANNUNCIATIONS & ALERTS

GMU 44 Message Advisories Alerts Window Message Comments HDG FAULT – AHRS1 magnetometer A fault has occurred in the GMU 44. Heading is flagged as invalid. The AHRS uses fault has occurred. GPS for backup mode operation. The G1000 system should be serviced. MANIFEST – GMU1 software The GMU 44 has incorrect software installed. The G1000 system should be serviced. mismatch. Communication halted. GDL 69 Message Advisories Alerts Window Message Comments GDL69 CONFIG – GDL 69 configura- GDL 69 configuration settings do not match those of backup configuration memory. tion error. Config service req’d. The G1000 system should be serviced. GDL69 FAIL – GDL 69 has failed. A failure has been detected in the GDL 69. The receiver is unavailable. The G1000 system should be serviced GDC 74A Message Advisories Alerts Window Message Comments GDC1 CONFIG – GDC1 configuration GDC 74A configuration settings do not match those of backup configuration error. Config service req’d. memory. The G1000 system should be serviced. MANIFEST – GDC1 software The GDC 74A has incorrect software installed. The G1000 system should be mismatch. Communication halted. serviced. BACKUP PATH – ADC1 using backup The GDC 74A is using a backup communications data path. The G1000 system data path. should be serviced when possible.

Miscellaneous Message Advisories Alerts Window Message Comments FPL WPT LOCK – Flight plan waypoint Upon power-up, the G1000 system detects that a stored flight plan waypoint is is locked. locked. This occurs when an aviation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags this message. This can also occur with user waypoints in a flight plan that is deleted. Remove the waypoint from the flight plan if it no longer exists in any database, OR update the waypoint name/identifier to reflect the new information.

12-14 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 12 – ANNUNCIATIONS & ALERTS

Miscellaneous Message Advisories (Cont.) Alerts Window Message Comments FPL WPT MOVE – Flight plan The system has detected that a waypoint coordinate has changed due to a new waypoint moved. aviation database update. Verify that stored flight plans contain correct waypoint locations. TIMER EXPIRD – Timer has expired. The system notifies the pilot that the timer has expired. DB CHANGE – Database changed. This occurs when a stored flight plan contains procedures that have been manually Verify user modified procedures. edited. This alert is issued only after an aviation database update. Verify that the user-modified procedures in stored flight plans are correct and up to date. FPL TRUNC – Flight plan has been This occurs when a newly installed aviation database eliminates an obsolete ap- truncated. proach or arrival used by a stored flight plan. The obsolete procedure is removed from the flight plan. Update flight plan with current arrival or approach. APPR VPROF – Approaching VNAV Aircraft is approaching VNAV profile. Prepare to climb or descend to meet VNAV profile. profile. APPR TRG ALT – Approaching target Aircraft is approaching target altitude. Prepare to level aircraft. altitude. LOCKED FPL – Cannot navigate locked This occurs when the pilot attempts to activate a stored flight plan that contains flight plan. locked waypoint. Remove locked waypoint from flight plan. Update flight plan with current waypoint. WPT ARRIVAL – Arriving at waypoint Arriving at waypoint [xxxx], where [xxxx] is the waypoint name. -[xxxx] STEEP TURN – Steep turn ahead. A steep turn is 15 seconds ahead. Prepare to turn. INSIDE ARSPC – Inside airspace. The aircraft is inside the airspace. ARSPC AHEAD – Airspace ahead less Special use airspace is ahead of aircraft. The aircraft will penetrate the airspace than 10 minutes. within 10 minutes. ARSPC NEAR – Airspace near and Special use airspace is near and ahead of the aircraft position. ahead. ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the aircraft position. than 2 nm. LEG UNSMOOTH – Flight plan leg will The approaching flight plan waypoints are too close to allow for smooth turns. not be smooth. Prepare for steep turns ahead and expect noticeable course deviations. APPR INACTV – Approach is not The system notifies the pilot that the loaded approach is not active. Activate ap- active. proach when required.

Garmin G1000 Cockpit Reference Guide for the DA40 12-15 SECTION 12 – ANNUNCIATIONS & ALERTS

Miscellaneous Message Advisories (Cont.) Alerts Window Message Comments SLCT AUTOSEQ – Select auto The system notifies the pilot to select auto-sequence mode. Press the OBS Softkey to sequence mode. deactivate the OBS mode. SLCT FREQ – Select appropriate The system notifies the pilot to load the approach frequency for the appropriate NAV frequency for approach. receiver. Select the correct frequency for the approach. SLCT NAV – Select NAV on CDI for The system notifies the pilot to set the CDI to the correct NAV receiver. Set the CDI approach. to the correct NAV receiver. NO WGS84 WPT – Non WGS 84 The selected waypoint [xxxx] does not use the WGS 84 datum. Cross-check position waypoint for navigation -[xxxx] with alternate navigation sources. TRAFFIC FAIL – Traffic device has The G1000 is no longer receiving data from the traffic system. The traffic device failed. should be serviced. STRMSCP FAIL – Stormscope has Stormscope has failed. The G1000 system should be serviced. failed. BACKUP PATH – Stormscope using Stormscope is using the backup communication path. The G1000 system should be backup path. serviced when possible.

12-16 Garmin G1000 Cockpit Reference Guide for the DA40 INDEX

A Auto-tuning 4-4 Engine display 3-1 Automatic squelch 4-3 ENGINE Softkey 3-1 Abnormal COM operation 11-2 Autopilot 6-1 – 6-3, 6-5 – 6-10, 6-12, Engine system 3-3 Activate a flight plan 8-3 6-13 Active flight plan 8-2 F ADF 1-5, 1-6, 4-3 B ADVISORY 12-1 FD 1-4, 12-4 Advisory alerts 12-3 Backcourse 6-11 FLC 1-4, 6-3, 6-7 AFCS 1-3, 6-1, 6-2 – 6-4, 6-6, 6-7, Barometric setting 2-4 Flight director 6-1 – 6-4, 6-6 – 6-10 6-9, 6-11 – 6-13, 12-4 Base reflectivity 10-2 Flight ID 4-5 Age 10-4 BKSP Softkey 4-5 Flight level change 1-4, 6-3, 6-7, 6-11, AHRS 12-13 BRG1 2-7 6-16 Aircraft alerts 12-3 BRG2 2-7 Flight Plan Catalog 9-1, 9-2 FPL key 1-3 AIRMET 10-3 C Airport frequency 7-6 Freezing level 10-3 Airport information 7-3 Caution 12-1, 12-2 Frequency toggle key 1-3, 4-3 Airspace alerts 7-9 CDI 2-7, 12-16 G Airspeed indicator 2-3 Cell movement 10-3 Airspeed trend vector 2-3 CLR key 1-3 GA 6-1, 6-3, 6-8, 6-9, 6-12 Alerting System 12-1 Codes (important) 4-5 Glideslope 6-3, 6-8, 6-9, 6-12 Alerts 12-1 Code selection 4-5 GMA 1347 1-1 Alert levels 12-2 CODE Softkey 4-5 Go Around 6-1, 6-3, 6-8, 6-9, 6-12, Altitude Hold 1-4 COM Frequency Window 4-1 6-19 Altitude hold 1-4, 6-3 – 6-8, 6-10 COM knob 4-3 Altitude trend vector 2-4 Controls 1-2, 4-1 H ALT knob 1-4 Control Wheel Steering 6-1, 6-3 HDG key 6-10 Annunciations 12-1 Create a new flight plan 8-3, 8-4 Heading hold 6-9 AP 1-4, 6-1 – 6-7, 6-9, 12-4 Create a new user waypoint 8-1 Heading indication 2-6, 2-7 Approaches 9-2 CWS 6-1, 6-3 – 6-9 Heading Select 1-3, 1-4, 6-9, 6-10 Approach activation 4-4 Cyclones 10-3 Heading Select Mode 6-10 Approach markers Cylinder Select 3-2 Headset(s) 5-2 Signal augmentation 5-2 CYL SLCT 3-2 Hijack code 4-5 Approach Mode 6-12 Horizontal situation indicator 2-5, 2-6 AP disconnect 6-1 D HSI 2-5 Arrivals 9-1 DEC FUEL 3-3 Hurricanes 10-3 ASSIST 3-2 Departures 9-1 Attitude indicator 2-3 Direct-to 7-1 I Audio alerting system 12-2 DME 1-6, 4-4 Audio panel 4-3, 5-1 ICAO 4-5 Dual CDU failure 11-2 Audio panel controls ID 4-3 ADF 5-2 E IDENT function 4-5 DME 5-2 INC FUEL 3-3 NAV1 5-2 Edit a flight plan 8-5 INTEG 2-8 NAV2 5-2 Emergency code 4-5 Interrogations 4-5

Garmin G1000 Cockpit Reference Guide for the DA40 Index-1 INDEX

K 7-8, 7-9, 8-1 Store Flight Plan 8-5 Nearest ARTCC & FSS frequencies 7-9 System annunciations 12-1, 12-5 Key(s) 1-4 NEXRAD 10-2 System message advisories 12-7 L O T Lean engine 3-2 OBS 2-8 TAS 12-13 Load approach 8-5 Obstacles 12-9, 12-10, 12-11 Terrain 10-6, 11-2, 12-9 Load a VOR frequency 7-8 Operation 5-2 Tornado 10-3 Load departure 8-4 Optional Traffic map page 10-5, 10-6, 10-7 Load the frequency for a controlling NAV radios 4-3 Transponder 4-5 agency 7-10 overspeed 6-2 Transponder Status bar 4-5 Load the nearest ARTCC frequency 7-9 Trim 6-1 Loss of communication code 4-5 P Tropical storms 10-3 M Page group icon 1-8 TX 4-3 PFD 1-1, 4-1, 4-4 V Manual Electric Trim 6-1 PIT 6-3 MAP 7-1 pitch axis modes 6-3 Vertical Deviation/Glideslope indica- Map panning 10-3 Pitch hold 1-4, 6-1, 6-3, 6-4, 6-8 tor 2-5 Marker beacon 2-5 Pitch Hold Mode 6-3 Vertical navigation profile 8-8 messages 12-1 PLAY key 5-4 Vertical speed 1-4, 2-5, 6-3, 6-6 Message advisories 12-2, 12-8 – 12- PROC key 1-3 Vertical Speed Bug 2-5 16 Vertical Speed Mode 6-6 MET 6-1, 6-3, 12-4 R VFR code 4-5 METAR 10-1, 10-3 Red pointer 2-3 VHF 4-1 MFD 1-1, 4-4 VOL/PUSH ID 4-2 Military interceptor operations code Remove departure, arrival, or approach 8-5 VOL/PUSH SQ 4-2, 4-3 4-5 Volume/squelch 5-3 Missed Approach 6-19 Replies 4-5 Reversionary mode 11-1 VS 1-4, 6-3, 6-6 Mistrim 12-4 Vspeeds 2-3 MKR/MUTE 5-2 Roll Axis Modes 6-2, 6-9 Mode selection softkeys 4-5 Roll Hold 6-9 W Morse code identifier 4-3 RST FUEL 3-3 RX indicator 4-3 WARN 2-8 N R indication 4-5 Warning 12-1, 12-2 Weather data link page 10-2 Nav/Com controls 4-1 S Weather product symbol 10-4 NAV1 5-2 Selected vertical speed 2-5 Weather product symbols 10-4 NAV2 5-2 Weather warnings 10-3 Navigation 7-1 Severe thunderstorm 10-3 SIGMET 10-3 Wind direction 10-3 Navigation Mode 6-11 Wind speed 10-3 Navigation status window 2-2 Slip/Skid indicator 2-3 NAV Frequency Window 4-1 Softkey function (MFD) 1-4, 1-7 X Nearest Airports Page 7-3, 7-5, 7-7, Speed ranges 2-3 Squelch 5-3 XPDR Softkey 4-5

Index-2 Garmin G1000 Cockpit Reference Guide for the DA40

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